<AcftExchangeFile>
<General Desc="Allgemeine Angaben">
<Type Desc="Flugzeugtyp" Unit="-">CeRAS</Type>
<Model Desc="Modell bzw. Ausfuehrung" Unit="-">CSR-02</Model>
</General>
<MassesAndLoadings Desc="-">
<MassBreakdown Desc="Mass breakdown">
<Wing Desc="Fluegelmasse und Schwerpunktlage des Massenelements, Airbus Chapter 10">
<Mass ToolLevel="1" Unit="kg">8288.967026</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
<y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
</RefPoint>
<CenterWing Desc="Masse der Fluegelstruktur (Skins, Spars, Ribs, Pylon attachments, LG supports), Airbus Ch. 10.0-4">
<Mass ToolLevel="1" Unit="kg">6063.492374</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
<y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
</RefPoint>
<EoW_CenterWingMassFactor Desc="Center wing mass factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_CenterWingMassFactor>
<EoW_AeroelasticFactor Desc="Aeroelastic (flutter) factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_AeroelasticFactor>
<EoW_TotalCenterWingMassFactor Desc="EoW_CenterWingMassFactor * EoW_AeroelasticFactor" ToolLevel="1" Unit="-">1</EoW_TotalCenterWingMassFactor>
</CenterWing>
<WingLEandTE Desc="Masse der Hochauftriebssysteme, Airbus Ch. 10.5-8">
<Mass ToolLevel="1" Unit="kg">2225.474652</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
<y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
</RefPoint>
<FixedLeadingEdge Desc="Mass of the complete fixed leading edge, Airbus Ch. 10.5">
<Mass ToolLevel="1" Unit="kg">282.297482</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
<y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
</RefPoint>
</FixedLeadingEdge>
<MovableLeadingEdge Desc="Mass of the complete movable leading edge, Airbus Ch. 10.6">
<Mass ToolLevel="1" Unit="kg">380.8095925</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
<y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
</RefPoint>
</MovableLeadingEdge>
<FixedTrailingEdge Desc="Mass of the fixed trailing edge, Airbus Ch. 10.7">
<Mass ToolLevel="1" Unit="kg">546.1954554</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
<y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
</RefPoint>
</FixedTrailingEdge>
<MovableTrailingEdge Desc="Mass of the movable trailing edge, Airbus Ch. 10.8">
<Mass ToolLevel="1" Unit="kg">1016.172122</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
<y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
</RefPoint>
</MovableTrailingEdge>
</WingLEandTE>
<Miscellaneous Desc="Restliche Fluegelmassenanteile, Airbus Ch. 10.9">
<Mass ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
<y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
</RefPoint>
</Miscellaneous>
</Wing>
<Fuselage Desc="Rumpfmasse und Schwerpunktlage des Massenelements, Airbus Chapter 11">
<Mass Desc="-" ToolLevel="1" Unit="kg">8482.604033</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
<y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Fuselage>
<Empennage Desc="Masse der Leitwerksgruppe und Schwerpunktlage des Massenelements">
<Mass Desc="Gesamtmasse der Leitwerksgruppe" ToolLevel="1" Unit="kg">1325.468005</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">33.95934635</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.654512598</h_Item>
</RefPoint>
<Tailplane Desc="Airbus Chapter 13">
<Mass ToolLevel="1" Unit="kg">759.3554913</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">34.25726239</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.654512598</h_Item>
</RefPoint>
</Tailplane>
<Fin Desc="Airbus Chapter 14">
<Mass Desc="-" ToolLevel="1" Unit="kg">566.1125139</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">33.55973642</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.654512598</h_Item>
</RefPoint>
</Fin>
</Empennage>
<LandingGear Desc="Fahrwerksmasse und Schwerpunktlage des Massenelements, Airbus Chapter 15">
<Mass Desc="-" ToolLevel="1" Unit="kg">2600.672138</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.45985449</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.413319125</h_Item>
</RefPoint>
<Gear Desc="Beschreibung des Bugfahrwerks" ID="NoseGear">
<Mass Desc="Mass of single gear" ToolLevel="1" Unit="kg">390.1008207</Mass>
<RefPoint Desc="Position of NoseGear CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">1.947356458</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">-1.978883883</h_Item>
</RefPoint>
<Strut>
<strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
<RefPoint Desc="position of strut CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Strut>
<SupportStrut>
<suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
<RefPoint Desc="position of suppStrut CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</SupportStrut>
<WheelGroupConnection>
<connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
<RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</WheelGroupConnection>
<WheelGroup>
<tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
<axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
<rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
<brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
</WheelGroup>
</Gear>
<Gear Desc="Beschreibung des aeusseren, rechten Hauptfahrwerks" ID="OuterRightMainGear">
<Mass Desc="Mass of single gear" ToolLevel="1" Unit="kg">1105.285659</Mass>
<RefPoint Desc="Position of OuterRightMainGear CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">17.84441297</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">-1.313513579</h_Item>
</RefPoint>
<Strut>
<strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
<RefPoint Desc="position of strut CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Strut>
<SupportStrut>
<suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
<RefPoint Desc="position of suppStrut CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</SupportStrut>
<WheelGroupConnection>
<connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
<RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</WheelGroupConnection>
<WheelGroup>
<tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
<axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
<rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
<brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
</WheelGroup>
</Gear>
<Gear Desc="Beschreibung des aeusseren, linken Hauptfahrwerks" ID="OuterLeftMainGear">
<Mass Desc="Mass of single gear" ToolLevel="1" Unit="kg">1105.285659</Mass>
<RefPoint Desc="Position of OuterLeftMainGear CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">17.84441297</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">-1.313513579</h_Item>
</RefPoint>
<Strut>
<strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
<RefPoint Desc="position of strut CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Strut>
<SupportStrut>
<suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
<RefPoint Desc="position of suppStrut CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</SupportStrut>
<WheelGroupConnection>
<connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
<RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</WheelGroupConnection>
<WheelGroup>
<tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
<axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
<rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
<brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
</WheelGroup>
</Gear>
<Gear Desc="Beschreibung des inneren, rechten Hauptfahrwerks" ID="InnerRightMainGear">
<Mass Desc="Mass of single gear" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="Position of InnerRightMainGear CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
<Strut>
<strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
<RefPoint Desc="position of strut CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Strut>
<SupportStrut>
<suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
<RefPoint Desc="position of suppStrut CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</SupportStrut>
<WheelGroupConnection>
<connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
<RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</WheelGroupConnection>
<WheelGroup>
<tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
<axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
<rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
<brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
</WheelGroup>
</Gear>
<Gear Desc="Beschreibung des inneren, linken Hauptfahrwerks" ID="InnerLeftMainGear">
<Mass Desc="Mass of single gear" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="Position of InnerLeftMainGear CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
<Strut>
<strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
<RefPoint Desc="position of strut CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Strut>
<SupportStrut>
<suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
<RefPoint Desc="position of suppStrut CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</SupportStrut>
<WheelGroupConnection>
<connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
<RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
<r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</WheelGroupConnection>
<WheelGroup>
<tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
<axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
<rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
<brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
</WheelGroup>
</Gear>
</LandingGear>
<Pylons Desc="Pylonmasse und Schwerpunktlage (aller Pylons), Airbus Chapter 16">
<Mass Desc="-" ToolLevel="1" Unit="kg">1302.156306</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.87054623</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.53285849</h_Item>
</RefPoint>
</Pylons>
<PowerUnit Desc="Masse und Schwerpunktlage der Triebwerksanlage, Airbus Group Power Unit">
<Mass Desc="Gesamtmasse der Gruppe Antriebsanlage" ToolLevel="1" Unit="kg">8513.660953</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.78507499</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.958381704</h_Item>
</RefPoint>
<Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="1">
<Mass Desc="-" ToolLevel="1" Unit="kg">4009.674109</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.49297931</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
</RefPoint>
<EngineDry Desc="Engine dry mass">
<Mass Desc="-" ToolLevel="1" Unit="kg">2748.88918</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.49297931</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
</RefPoint>
</EngineDry>
<Nacelle Desc="Nacelle mass">
<Mass Desc="-" ToolLevel="1" Unit="kg">713.6948535</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.49297931</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
</RefPoint>
</Nacelle>
<OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
<Mass Desc="-" ToolLevel="1" Unit="kg">547.0900758</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.49297931</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
</RefPoint>
</OtherSystems>
<Prop Desc="Propeller mass">
<Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Prop>
</Engine>
<Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="2">
<Mass Desc="-" ToolLevel="1" Unit="kg">4009.674109</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.49297931</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
</RefPoint>
<EngineDry Desc="Engine dry mass">
<Mass Desc="-" ToolLevel="1" Unit="kg">2748.88918</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.49297931</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
</RefPoint>
</EngineDry>
<Nacelle Desc="Nacelle mass">
<Mass Desc="-" ToolLevel="1" Unit="kg">713.6948535</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.49297931</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
</RefPoint>
</Nacelle>
<OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
<Mass Desc="-" ToolLevel="1" Unit="kg">547.0900758</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.49297931</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
</RefPoint>
</OtherSystems>
<Prop Desc="Propeller mass">
<Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Prop>
</Engine>
<Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="3">
<Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
<EngineDry Desc="Engine dry mass">
<Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</EngineDry>
<Nacelle Desc="Nacelle mass">
<Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Nacelle>
<OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
<Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</OtherSystems>
<Prop Desc="Propeller mass">
<Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Prop>
</Engine>
<Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="4">
<Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
<EngineDry Desc="Engine dry mass">
<Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</EngineDry>
<Nacelle Desc="Nacelle mass">
<Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Nacelle>
<OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
<Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</OtherSystems>
<Prop Desc="Propeller mass">
<Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Prop>
</Engine>
<BleedAirSystem Desc="Airbus Chapter 21, ATA36">
<Mass Desc="-" ToolLevel="1" Unit="kg">172.6795332</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.05413654</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.27103384</h_Item>
</RefPoint>
</BleedAirSystem>
<EngineControls Desc="Airbus Chapter 22">
<Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</EngineControls>
<FuelSystem Desc="Airbus Chapter 25, ATA28">
<Mass Desc="-" ToolLevel="1" Unit="kg">321.6332021</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
</RefPoint>
</FuelSystem>
</PowerUnit>
<Systems Desc="Systemmasse und Schwerpunktlage des Massenelements, Airbus Group Systems">
<Mass Desc="Gesamtmasse der Systemgruppe" ToolLevel="1" Unit="kg">5355.445849</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.39637449</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-0.5741904671</h_Item>
</RefPoint>
<APU Desc="Airbus Chapter 30, ATA49">
<Mass Desc="-" ToolLevel="1" Unit="kg">254.7995941</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">35.65115779</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</APU>
<HydraulicGeneration Desc="Airbus Chapter 31, ATA 29">
<Mass Desc="-" ToolLevel="1" Unit="kg">184.4172612</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.05413654</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.27103384</h_Item>
</RefPoint>
</HydraulicGeneration>
<HydraulicDistribution Desc="Airbus Chapter 32, ATA 29">
<Mass Desc="-" ToolLevel="1" Unit="kg">805.6612438</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.05413654</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.27103384</h_Item>
</RefPoint>
</HydraulicDistribution>
<AirConditioning Desc="Airbus Chapter 33, ATA21">
<Mass Desc="-" ToolLevel="1" Unit="kg">717.7462397</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.05413654</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.27103384</h_Item>
</RefPoint>
</AirConditioning>
<DeIcing Desc="Airbus Chapter 34, ATA30">
<Mass Desc="-" ToolLevel="1" Unit="kg">42.30906964</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</DeIcing>
<FireProtection Desc="Airbus Chapter 35, ATA26">
<Mass Desc="-" ToolLevel="1" Unit="kg">94.97439103</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</FireProtection>
<FlightControls Desc="Airbus Chapter 36, ATA27">
<Mass Desc="-" ToolLevel="1" Unit="kg">711.5018356</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.05413654</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.27103384</h_Item>
</RefPoint>
<Roll Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.0">
<Mass Desc="-" ToolLevel="1" Unit="kg">43.35817647</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Roll>
<Yaw Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.1">
<Mass Desc="-" ToolLevel="1" Unit="kg">94.98684287</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Yaw>
<Pitch Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.2">
<Mass Desc="-" ToolLevel="1" Unit="kg">33.35895545</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Pitch>
<MovableHorizontalTail Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.3">
<Mass Desc="-" ToolLevel="1" Unit="kg">64.77541722</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</MovableHorizontalTail>
<Flaps Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.4">
<Mass Desc="-" ToolLevel="1" Unit="kg">147.1812978</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Flaps>
<SpoilersAirbrakesLiftdumpers Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.5">
<Mass Desc="-" ToolLevel="1" Unit="kg">39.74320013</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</SpoilersAirbrakesLiftdumpers>
<Slats Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.6">
<Mass Desc="-" ToolLevel="1" Unit="kg">145.7975785</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Slats>
<CommonInstallation Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.7">
<Mass Desc="-" ToolLevel="1" Unit="kg">142.3003671</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</CommonInstallation>
</FlightControls>
<Instruments Desc="Airbus Chapter 37, ATA31">
<Mass ToolLevel="1" Unit="kg">85.52867064</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">4.125269051</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Instruments>
<AutomaticFlightSystem Desc="Airbus Chapter 38, ATA 22">
<Mass ToolLevel="1" Unit="kg">138.9840898</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.51238234</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</AutomaticFlightSystem>
<Navigation Desc="Airbus Chapter 39, ATA34">
<Mass Desc="-" ToolLevel="1" Unit="kg">566.627443</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.51238234</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Navigation>
<Communication Desc="Airbus Chapter 40, ATA23">
<Mass Desc="-" ToolLevel="1" Unit="kg">277.9681796</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.51238234</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Communication>
<ElectricalGeneration Desc="Airbus Chapter 41, ATA24">
<Mass Desc="-" ToolLevel="1" Unit="kg">779.0134574</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</ElectricalGeneration>
<ElectricalDistribution Desc="Airbus Chapter 42, ATA24">
<Mass Desc="-" ToolLevel="1" Unit="kg">695.9143735</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</ElectricalDistribution>
</Systems>
<Furnishings Desc="Furnishingmasse und Schwerpunktlage des Massenelements, Airbus Group Furnishings">
<Mass Desc="Gesamtmasse der Furnishinggruppe" ToolLevel="1" Unit="kg">3108.708964</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
<Furnishing Desc="Airbus Chapter 50, ATA25">
<Mass Desc="-" ToolLevel="1" Unit="kg">2452.022285</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Furnishing>
<FixedEmergencyOxygen Desc="Airbus Chapter 51, ATA35">
<Mass Desc="-" ToolLevel="1" Unit="kg">98.464</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</FixedEmergencyOxygen>
<Lighting Desc="Airbus Chapter 52, ATA33">
<Mass Desc="-" ToolLevel="1" Unit="kg">268.2126788</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</Lighting>
<WaterInstallation Desc="Airbus Chapter 53, ATA38">
<Mass Desc="-" ToolLevel="1" Unit="kg">290.01</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</WaterInstallation>
</Furnishings>
<OperatorsItems Desc="Masse der Betreiberausstattung und Schwerpunktlage des Massenelements, Airbus Group Operator Items">
<Mass Desc="Gesamtmasse der Operators Items Gruppe" ToolLevel="1" Unit="kg">3331.623637</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.6792334</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
<OperatorEquipment Desc="Airbus Chapter 60 (fixed equipment, vorher Standard Items)">
<Mass Desc="-" ToolLevel="1" Unit="kg">1581.073637</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.71467966</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</OperatorEquipment>
<OperationalEquipment Desc="Airbus Chapter 61 (movable equipment)">
<Mass Desc="-" ToolLevel="1" Unit="kg">1750.55</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.84084522</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</OperationalEquipment>
</OperatorsItems>
<NotAllocated Desc="Nicht zugeordnete Massenanteile und Schwerpunktlage des Massenelements">
<Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
<RefPoint Desc="position of mass item to global point of reference">
<r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
<y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
<h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
</RefPoint>
</NotAllocated>
</MassBreakdown>
<MTM Desc="Maximum Taxi Mass" ToolLevel="1" Unit="kg">0</MTM>
<MLM Desc="Maximum Landing Mass" ToolLevel="1" Unit="kg">66724.81066</MLM>
<MTOM Desc="Maximum Take-Off Mass" ToolLevel="3" Unit="kg">79148.59668</MTOM>
<MRM Desc="Maximum Ramp Mass" ToolLevel="1" Unit="kg">0</MRM>
<MME Desc="Manufacturing Mass Empty" ToolLevel="1" Unit="kg">38977.68327</MME>
<OME Desc="Operating Mass Empty" ToolLevel="1" Unit="kg">42309.30691</OME>
<MZFM Desc="Maximum Zero Fuel Mass" ToolLevel="1" Unit="kg">62309.30691</MZFM>
<MaximumPayload Desc="Maximale Nutzlast" ToolLevel="1" Unit="kg">20000</MaximumPayload>
<MaximumUsableFuel Desc="Benutzbare Kraftstoffmasse" ToolLevel="1" Unit="kg">32478.96446</MaximumUsableFuel>
<WingLoading Desc="Fluegelflaechenlast" ToolLevel="1" Unit="kg/m2">625.8366729</WingLoading>
<ThrustToWeight Desc="Schubkraft (kN) zu Gewichtskrafthaeltnis (kN)" ToolLevel="1" Unit="-">0.3320609465</ThrustToWeight>
<PowerToWeight Desc="Leistungsgewicht" ToolLevel="1" Unit="kW/kg">0</PowerToWeight>
<MassMomentsOfInertia Desc="Mass moment of inertia (MMoI)">
<DesignPoint Desc="MMoI at Designpoint">
<Jxx Desc="MMoI x-axis" ToolLevel="1" Unit="kg*m2">1200828.866</Jxx>
<Jyy Desc="MMoI y-axis" ToolLevel="1" Unit="kg*m2">3139142.531</Jyy>
<Jzz Desc="MMoI z-axis" ToolLevel="1" Unit="kg*m2">4166372.541</Jzz>
<Jxy Desc="MMoI xy-axis (deviation)" ToolLevel="1" Unit="kg*m2">0</Jxy>
<Jxz Desc="MMoI xz-axis (deviation)" ToolLevel="1" Unit="kg*m2">0</Jxz>
<Jyz Desc="MMoI yz-axis (deviation)" ToolLevel="1" Unit="kg*m2">0</Jyz>
</DesignPoint>
</MassMomentsOfInertia>
<CentreOfGravityRange Desc="Schwerpunktsgrenzen">
<TrimRefPt Desc="Schwerpunktlage fuer CM-Berechnung und Trimmung im Reiseflug">
<h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-0.7482016769</h>
<r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.80339635</r>
<y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y>
</TrimRefPt>
<ForwardLimit Desc="Vorderste Schwerpunktlage">
<h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-0.9750336151</h>
<r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.67440503</r>
<y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y>
</ForwardLimit>
<AftLimit Desc="Hinterste Schwerpunktlage">
<h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-0.9992954046</h>
<r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.88886532</r>
<y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y>
</AftLimit>
</CentreOfGravityRange>
</MassesAndLoadings>
<Geometry Desc="Geometriebeschreibung">
<UsedElements Desc="Liste der verwendeten Geometrieelemente">
<LiftingSurfaces Desc="Anzahl der verwendeten Elemente LiftingSurface" ToolLevel="1">2</LiftingSurfaces>
<LiftingSurface Desc="Name des verwendeten LiftingSurface-Elements" ID="1" ToolLevel="1" Unit="-">MainWing</LiftingSurface>
<LiftingSurface Desc="Name des verwendeten LiftingSurface-Elements" ID="2" ToolLevel="1" Unit="-">Stabiliser</LiftingSurface>
<VerticalSurfaces Desc="Anzahl der verwendeten Elemente VerticalSurface" ToolLevel="1">1</VerticalSurfaces>
<VerticalSurface Desc="Name des verwendeten VerticalSurface-Elements" ID="1" ToolLevel="1" Unit="-">Fin</VerticalSurface>
<VerticalSurface Desc="Name des verwendeten VerticalSurface-Elements" ID="2" ToolLevel="1" Unit="-">0</VerticalSurface>
<Fuselages Desc="Anzahl der verwendeten Elemente Fuselage" ToolLevel="1">1</Fuselages>
<Fuselage Desc="Name des verwendeten Fuselage-Elements" ID="1" ToolLevel="1" Unit="-">Fuselage</Fuselage>
<Nacelles Desc="Anzahl der verwendeten Elemente Nacelle" ToolLevel="1">2</Nacelles>
<Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="1" ToolLevel="1" Unit="-">InnerRightWingNacelle</Nacelle>
<Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="2" ToolLevel="1" Unit="-">InnerLeftWingNacelle</Nacelle>
<Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="3" ToolLevel="1" Unit="-">0</Nacelle>
<Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="4" ToolLevel="1" Unit="-">0</Nacelle>
<Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="5" ToolLevel="1" Unit="-">0</Nacelle>
<Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="6" ToolLevel="1" Unit="-">0</Nacelle>
<Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="7" ToolLevel="1" Unit="-">0</Nacelle>
<Pylons Desc="Anzahl der verwendeten Elemente Pylon" ToolLevel="1">2</Pylons>
<Pylon Desc="Name des verwendeten Pylon-Elements" ID="1" ToolLevel="1" Unit="-">InnerRightWingPylon</Pylon>
<Pylon Desc="Name des verwendeten Pylon-Elements" ID="2" ToolLevel="1" Unit="-">InnerLeftWingPylon</Pylon>
<Pylon Desc="Name des verwendeten Pylon-Elements" ID="3" ToolLevel="1" Unit="-">0</Pylon>
<Pylon Desc="Name des verwendeten Pylon-Elements" ID="4" ToolLevel="1" Unit="-">0</Pylon>
<Pylon Desc="Name des verwendeten Pylon-Elements" ID="5" ToolLevel="1" Unit="-">0</Pylon>
<Pylon Desc="Name des verwendeten Pylon-Elements" ID="6" ToolLevel="1" Unit="-">0</Pylon>
<Gears Desc="Anzahl der verwendeten Elemente Gear" ToolLevel="1">3</Gears>
<Gear Desc="Name des verwendeten Gear-Elements" ID="1" ToolLevel="1" Unit="-">NoseGear</Gear>
<Gear Desc="Name des verwendeten Gear-Elements" ID="2" ToolLevel="1" Unit="-">OuterRightMainGear</Gear>
<Gear Desc="Name des verwendeten Gear-Elements" ID="3" ToolLevel="1" Unit="-">OuterLeftMainGear</Gear>
<Gear Desc="Name des verwendeten Gear-Elements" ID="4" ToolLevel="1" Unit="-">0</Gear>
<Gear Desc="Name des verwendeten Gear-Elements" ID="5" ToolLevel="1" Unit="-">0</Gear>
</UsedElements>
<LiftingSurface Desc="Beschreibung des Hauptfluegels" ID="MainWing">
<SurfaceRefPoint Desc="position of wing to global point of reference">
<r_Surface Desc="Position of the wing to global point of reference in x-direction" ToolLevel="1" Unit="m">12.51238234</r_Surface>
<y_Surface Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Surface>
<h_Surface Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.27103384</h_Surface>
</SurfaceRefPoint>
<SurfaceParameters Desc="Parametric description of lifting surface geometry">
<Symmetric Desc="1:= symmetric wing / 0 := asymmetric wing" ToolLevel="1" Unit="-">1</Symmetric>
<RelChordRefForRotation Desc="Rel. Chordtiefe: Ref.-Pkt. fuer Verwindg. u. V-Stellg." ToolLevel="1" Unit="-">0</RelChordRefForRotation>
<i_Surface Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="deg">0</i_Surface>
<SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">200</SectionPoints>
<HalfSurfaceDescription Desc="Parameters of right wing (or both wings, if symmetric)" ID="1">
<HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">2</HalfSurfaceSegments>
<HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\F15_15.dat</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\F15_12.dat</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">7.083508401</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">4.434391811</l_o_Segment>
<s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">5.199184069</s_Segment>
<epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">2.091406079</nu_Segment>
<phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">26.99999996</phi_Segment>
<l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.11</l_rel_i_FrontSpar>
<l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.55</l_rel_i_RearSpar>
<l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.16</l_rel_o_FrontSpar>
<l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.65</l_rel_o_RearSpar>
</HalfSurfaceSegment>
<HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="Surface">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\F15_12.dat</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\F15_11.dat</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">4.434391811</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.053794453</l_o_Segment>
<s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">12.1314295</s_Segment>
<epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">2.374274265</nu_Segment>
<phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">26.99999996</phi_Segment>
<l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.16</l_rel_i_FrontSpar>
<l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.65</l_rel_i_RearSpar>
<l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.27</l_rel_o_FrontSpar>
<l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.55</l_rel_o_RearSpar>
</HalfSurfaceSegment>
<HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="3" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
<l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
<l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
<l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
<l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
</HalfSurfaceSegment>
<ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
<TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">8</TEDevices>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Fowler</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.1168298891</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.2</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.294</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">45</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Fowler</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.306</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.78</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">45</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Aileron</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.8</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.98</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerGround</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2054149445</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.125</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.25</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.294</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.306</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.4195</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.4195</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.533</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.533</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.6465</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.6465</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.76</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">1</LEDevices>
<LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
<Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">Slat</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.1168298891</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.11</l_rel_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.27</l_rel_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">35</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</LEDevice>
</ControlDeviceSetup>
</HalfSurfaceDescription>
<HalfSurfaceDescription Desc="Parameters of left wing (if asymmetric)" ID="2">
<HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">0</HalfSurfaceSegments>
<HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
<l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
<l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
<l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
<l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
</HalfSurfaceSegment>
<ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
<TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">0</TEDevices>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices>
<LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
<Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</LEDevice>
</ControlDeviceSetup>
</HalfSurfaceDescription>
</SurfaceParameters>
</LiftingSurface>
<LiftingSurface Desc="Beschreibung des Hoehenleitwerks" ID="Stabiliser">
<SurfaceRefPoint Desc="position of wing to global point of reference">
<r_Surface Desc="Position of the wing to global point of reference in x-direction" ToolLevel="1" Unit="m">31.6591417</r_Surface>
<y_Surface Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Surface>
<h_Surface Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">1.654512598</h_Surface>
</SurfaceRefPoint>
<SurfaceParameters Desc="Parametric description of lifting surface geometry">
<Symmetric Desc="1:= symmetric wing / 0 := asymmetric wing" ToolLevel="1" Unit="-">1</Symmetric>
<RelChordRefForRotation Desc="Rel. Chordtiefe: Ref.-Pkt. fuer Verwindg. u. V-Stellg." ToolLevel="1" Unit="-">0</RelChordRefForRotation>
<i_Surface Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="deg">-1.250900566</i_Surface>
<SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
<HalfSurfaceDescription Desc="Parameters of right wing (or both wings, if symmetric)" ID="1">
<HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">1</HalfSurfaceSegments>
<HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.992016088</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.123933623</l_o_Segment>
<s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">6.439701701</s_Segment>
<epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">31.99999988</phi_Segment>
<l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.15</l_rel_i_FrontSpar>
<l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.65</l_rel_i_RearSpar>
<l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.3</l_rel_o_FrontSpar>
<l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.55</l_rel_o_RearSpar>
</HalfSurfaceSegment>
<HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
<l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
<l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
<l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
<l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
</HalfSurfaceSegment>
<ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
<TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">1</TEDevices>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
<Type Desc="Typ der Hinterkantenflaeche (Elevator)" ToolLevel="1">Elevator</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg>
</DeflectionAngle>
</TEDevice>
<LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices>
<LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
<Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</LEDevice>
</ControlDeviceSetup>
</HalfSurfaceDescription>
<HalfSurfaceDescription Desc="Parameters of left wing (if asymmetric)" ID="2">
<HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">0</HalfSurfaceSegments>
<HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
<l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
<l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
<l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
<l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
</HalfSurfaceSegment>
<ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
<TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">0</TEDevices>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8">
<Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</TEDevice>
<LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices>
<LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
<Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
</DeflectionAngle>
</LEDevice>
</ControlDeviceSetup>
</HalfSurfaceDescription>
</SurfaceParameters>
</LiftingSurface>
<VerticalSurface Desc="Beschreibung des Seitenleitwerks" ID="Fin">
<SurfaceRefPoint Desc="Referenzpunkt der vertikalen Steuerflaeche">
<r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">29.86369528</r_Surface>
<y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
<h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">1.654512598</h_Surface>
</SurfaceRefPoint>
<SurfaceParameters Desc="Parametric description of vertical surface geometry">
<SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
<SurfaceSegments Desc="Number of segments in this vertical surface" ToolLevel="1">1</SurfaceSegments>
<SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">5.787462516</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.531274612</l_o_Segment>
<s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">6.952800274</s_Segment>
<phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">38.99999987</phi_Segment>
<l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
<l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
<l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
<l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
</SurfaceSegment>
<SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
<phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
<l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
<l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
<l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
<l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
</SurfaceSegment>
<SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="3" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
<phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
<l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
<l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
<l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
<l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
</SurfaceSegment>
<ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
<TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">1</TEDevices>
<TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
<Type Desc="Typ der Hinterkantenflaeche (Rudder)" ToolLevel="1">Rudder</Type>
<s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2</s_rel_i>
<l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
<s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o>
<l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
<DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
<FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos>
<FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg>
</DeflectionAngle>
</TEDevice>
</ControlDeviceSetup>
</SurfaceParameters>
</VerticalSurface>
<Fuselage Desc="Beschreibung des Rumpfes" ID="Fuselage">
<FuselageRefPoint Desc="position of the fuselage nose refpoint to global point of reference">
<r_Fuselage Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Fuselage>
<y_Fuselage Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Fuselage>
<h_Fuselage Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Fuselage>
</FuselageRefPoint>
<FuselageParameters Desc="parametric description of the fuselage">
<NoseDescription>
<NoseSegments Desc="No of nose segments" ToolLevel="1">9</NoseSegments>
<TipSegment>
<h_Tip Desc="offset of nosetip" ToolLevel="1" Unit="m">-0.5232505048</h_Tip>
</TipSegment>
<NoseSegment ID="1">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0.6219072875</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0.647944796</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.06445732892</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.5232505048</deltah_Segment>
</NoseSegment>
<NoseSegment ID="2">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.232171749</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.283759313</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.1933719868</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.4278783272</deltah_Segment>
</NoseSegment>
<NoseSegment ID="3">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.81877794</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.894925056</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.3222866446</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.3362034659</deltah_Segment>
</NoseSegment>
<NoseSegment ID="4">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">2.368913086</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">2.468092813</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.4512013025</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.2502283023</deltah_Segment>
</NoseSegment>
<NoseSegment ID="5">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">2.868421677</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">2.988514422</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.5801159603</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.1721650609</deltah_Segment>
</NoseSegment>
<NoseSegment ID="6">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.301028172</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.439232935</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.7090306182</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.1045572839</deltah_Segment>
</NoseSegment>
<NoseSegment ID="7">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.6471193</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.799813925</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.837945276</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.05047013554</deltah_Segment>
</NoseSegment>
<NoseSegment ID="8">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.881644273</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.044157799</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.9668599339</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.01381855438</deltah_Segment>
</NoseSegment>
<NoseSegment ID="9">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.970066</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.136281495</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.095774592</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0</deltah_Segment>
</NoseSegment>
</NoseDescription>
<MidSectionDescription>
<MidSectionSegments Desc="No of mid-segment segments" ToolLevel="1">1</MidSectionSegments>
<MidSectionSegment ID="1">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.970066</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.136281495</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">16.76076782</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0</deltah_Segment>
</MidSectionSegment>
<MidSectionSegment ID="2">
<SegmentPointData ToolLevel="1">0</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0</deltah_Segment>
</MidSectionSegment>
</MidSectionDescription>
<TailDescription>
<TailSegments Desc="No of tail segments" ToolLevel="1">7</TailSegments>
<TailSegment ID="1">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.970066</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.074891643</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.72542446</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.03069492579</deltah_Segment>
</TailSegment>
<TailSegment ID="2">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.970066</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.889781167</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.72542446</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.1232501637</deltah_Segment>
</TailSegment>
<TailSegment ID="3">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.892703799</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.578053688</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.72542446</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.2791139033</deltah_Segment>
</TailSegment>
<TailSegment ID="4">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.618301624</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.143415874</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.72542446</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.4964328104</deltah_Segment>
</TailSegment>
<TailSegment ID="5">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.142809701</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">2.681089784</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.72542446</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.7275958556</deltah_Segment>
</TailSegment>
<TailSegment ID="6">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.985033</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.754173041</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">3.459300377</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">1.191054227</deltah_Segment>
</TailSegment>
<TailSegment ID="7">
<SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
<w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0.827256299</w_Segment>
<h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0.827256299</h_Segment>
<l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">3.459300377</l_Segment>
<deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">1.654512598</deltah_Segment>
</TailSegment>
</TailDescription>
</FuselageParameters>
</Fuselage>
<Nacelle Desc="Beschreibung der inneren rechten Triebwerksgondel" ID="InnerRightWingNacelle">
<NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
<r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.30681609</r_Nacelle>
<y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">5.49297931</y_Nacelle>
<h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-3.072020922</h_Nacelle>
</NacelleRefPoint>
<NacelleParameters Desc="parametric description of the nacelle">
<i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
<Points Desc="No of points describing the section" ToolLevel="1">20</Points>
<Segments Desc="No of segments" ToolLevel="1">2</Segments>
<InletSegment>
<SegmentPointData ToolLevel="1">geometryData\nacelle.dat</SegmentPointData>
<w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_Inlet>
<h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_Inlet>
<l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.6776753197</l_Inlet>
</InletSegment>
<NacelleSegment ID="1">
<InnerSegmentPointData ToolLevel="1">geometryData\nacelle.dat</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">geometryData\nacelle.dat</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.471029026</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.861475931</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">1.355350639</l_Segment>
</NacelleSegment>
<NacelleSegment ID="2">
<InnerSegmentPointData ToolLevel="1">geometryData\nacelle.dat</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">geometryData\nacelle.dat</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.471029026</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.861475931</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.6776753197</l_Segment>
</NacelleSegment>
<NacelleSegment ID="3">
<InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
</NacelleSegment>
<NacelleSegment ID="4">
<InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
</NacelleSegment>
<ExitSegment>
<SegmentPointData ToolLevel="1">geometryData\nacelle.dat</SegmentPointData>
<h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_Exit>
<w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_Exit>
</ExitSegment>
</NacelleParameters>
<EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
</Nacelle>
<Nacelle Desc="Beschreibung der inneren linken Triebwerksgondel" ID="InnerLeftWingNacelle">
<NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
<r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.30681609</r_Nacelle>
<y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-5.49297931</y_Nacelle>
<h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-3.072020922</h_Nacelle>
</NacelleRefPoint>
<NacelleParameters Desc="parametric description of the nacelle">
<i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
<Points Desc="No of points describing the section" ToolLevel="1">20</Points>
<Segments Desc="No of segments" ToolLevel="1">2</Segments>
<InletSegment>
<SegmentPointData ToolLevel="1">geometryData\nacelle.dat</SegmentPointData>
<w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_Inlet>
<h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_Inlet>
<l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.6776753197</l_Inlet>
</InletSegment>
<NacelleSegment ID="1">
<InnerSegmentPointData ToolLevel="1">geometryData\nacelle.dat</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">geometryData\nacelle.dat</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.471029026</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.861475931</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">1.355350639</l_Segment>
</NacelleSegment>
<NacelleSegment ID="2">
<InnerSegmentPointData ToolLevel="1">geometryData\nacelle.dat</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">geometryData\nacelle.dat</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.471029026</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.861475931</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.6776753197</l_Segment>
</NacelleSegment>
<NacelleSegment ID="3">
<InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
</NacelleSegment>
<NacelleSegment ID="4">
<InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
</NacelleSegment>
<ExitSegment>
<SegmentPointData ToolLevel="1">geometryData\nacelle.dat</SegmentPointData>
<h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_Exit>
<w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_Exit>
</ExitSegment>
</NacelleParameters>
<EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
</Nacelle>
<Nacelle Desc="Beschreibung der aeusseren rechten Triebwerksgondel" ID="OuterRightWingNacelle">
<NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
<r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
<y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
<h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
</NacelleRefPoint>
<NacelleParameters Desc="parametric description of the nacelle">
<i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
<Points Desc="No of points describing the section" ToolLevel="1">0</Points>
<Segments Desc="No of segments" ToolLevel="1">0</Segments>
<InletSegment>
<SegmentPointData ToolLevel="1">0</SegmentPointData>
<w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
<h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
<l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
</InletSegment>
<NacelleSegment ID="1">
<InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
</NacelleSegment>
<NacelleSegment ID="2">
<InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
</NacelleSegment>
<ExitSegment>
<SegmentPointData ToolLevel="1">0</SegmentPointData>
<h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
<w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
</ExitSegment>
</NacelleParameters>
<EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
</Nacelle>
<Nacelle Desc="Beschreibung der aeusseren linken Triebwerksgondel" ID="OuterLeftWingNacelle">
<NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
<r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
<y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
<h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
</NacelleRefPoint>
<NacelleParameters Desc="parametric description of the nacelle">
<i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
<Points Desc="No of points describing the section" ToolLevel="1">0</Points>
<Segments Desc="No of segments" ToolLevel="1">0</Segments>
<InletSegment>
<SegmentPointData ToolLevel="1">0</SegmentPointData>
<w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
<h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
<l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
</InletSegment>
<NacelleSegment ID="1">
<InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
</NacelleSegment>
<NacelleSegment ID="2">
<InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
</NacelleSegment>
<ExitSegment>
<SegmentPointData ToolLevel="1">0</SegmentPointData>
<h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
<w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
</ExitSegment>
</NacelleParameters>
<EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
</Nacelle>
<Nacelle Desc="Beschreibung der rechten Hecktriebwerksgondel" ID="RightFuselageNacelle">
<NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
<r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
<y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
<h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
</NacelleRefPoint>
<NacelleParameters Desc="parametric description of the nacelle">
<i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
<Points Desc="No of points describing the section" ToolLevel="1">0</Points>
<Segments Desc="No of segments" ToolLevel="1">0</Segments>
<InletSegment>
<SegmentPointData ToolLevel="1">0</SegmentPointData>
<w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
<h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
<l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
</InletSegment>
<NacelleSegment ID="1">
<InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
</NacelleSegment>
<NacelleSegment ID="2">
<InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
</NacelleSegment>
<ExitSegment>
<SegmentPointData ToolLevel="1">0</SegmentPointData>
<h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
<w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
</ExitSegment>
</NacelleParameters>
<EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
</Nacelle>
<Nacelle Desc="Beschreibung der linken Hecktriebwerksgondel" ID="LeftFuselageNacelle">
<NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
<r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
<y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
<h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
</NacelleRefPoint>
<NacelleParameters Desc="parametric description of the nacelle">
<i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
<Points Desc="No of points describing the section" ToolLevel="1">0</Points>
<Segments Desc="No of segments" ToolLevel="1">0</Segments>
<InletSegment>
<SegmentPointData ToolLevel="1">0</SegmentPointData>
<w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
<h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
<l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
</InletSegment>
<NacelleSegment ID="1">
<InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
</NacelleSegment>
<NacelleSegment ID="2">
<InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
</NacelleSegment>
<ExitSegment>
<SegmentPointData ToolLevel="1">0</SegmentPointData>
<h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
<w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
</ExitSegment>
</NacelleParameters>
<EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
</Nacelle>
<Nacelle Desc="Beschreibung der in das SLW integrierten Triebwerksgondel" ID="FinNacelle">
<NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
<r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
<y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
<h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
</NacelleRefPoint>
<NacelleParameters Desc="parametric description of the nacelle">
<i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
<Points Desc="No of points describing the section" ToolLevel="1">0</Points>
<Segments Desc="No of segments" ToolLevel="1">0</Segments>
<InletSegment>
<SegmentPointData ToolLevel="1">0</SegmentPointData>
<w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
<h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
<l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
</InletSegment>
<NacelleSegment ID="1">
<InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
</NacelleSegment>
<NacelleSegment ID="2">
<InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
<OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
<w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
<w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
<h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
<h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
<l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
</NacelleSegment>
<ExitSegment>
<SegmentPointData ToolLevel="1">0</SegmentPointData>
<h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
<w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
</ExitSegment>
</NacelleParameters>
<EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
</Nacelle>
<Pylon Desc="Beschreibung des Pylons" ID="InnerRightWingPylon">
<SurfaceRefPoint Desc="Referenzpunkt des Pylons">
<r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.57788621</r_Surface>
<y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">5.49297931</y_Surface>
<h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-3.072020922</h_Surface>
</SurfaceRefPoint>
<SurfaceParameters Desc="Parametric description of pylon geometry">
<SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
<SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">2</SurfaceSegments>
<SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="Surface">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.252841535</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">4.066051918</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">1.201819891</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
<SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="Surface">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">4.066051918</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">2.110599868</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0.8012132607</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">71.83066751</phi_Segment>
</SurfaceSegment>
<SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
</SurfaceParameters>
</Pylon>
<Pylon Desc="Beschreibung des Pylons" ID="InnerLeftWingPylon">
<SurfaceRefPoint Desc="Referenzpunkt des Pylons">
<r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.57788621</r_Surface>
<y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">-5.49297931</y_Surface>
<h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-3.072020922</h_Surface>
</SurfaceRefPoint>
<SurfaceParameters Desc="Parametric description of pylon geometry">
<SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
<SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">2</SurfaceSegments>
<SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="Surface">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.252841535</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">4.066051918</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">1.201819891</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
<SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="Surface">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">4.066051918</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">2.110599868</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0.8012132607</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">71.83066751</phi_Segment>
</SurfaceSegment>
<SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
</SurfaceParameters>
</Pylon>
<Pylon Desc="Beschreibung des Pylons" ID="OuterRightWingPylon">
<SurfaceRefPoint Desc="Referenzpunkt des Pylons">
<r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
<y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
<h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
</SurfaceRefPoint>
<SurfaceParameters Desc="Parametric description of pylon geometry">
<SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
<SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
<SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
<SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
<SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
</SurfaceParameters>
</Pylon>
<Pylon Desc="Beschreibung des Pylons" ID="OuterLeftWingPylon">
<SurfaceRefPoint Desc="Referenzpunkt des Pylons">
<r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
<y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
<h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
</SurfaceRefPoint>
<SurfaceParameters Desc="Parametric description of pylon geometry">
<SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
<SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
<SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
<SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
<SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
</SurfaceParameters>
</Pylon>
<Pylon Desc="Beschreibung des Pylons" ID="RightFuselagePylon">
<SurfaceRefPoint Desc="Referenzpunkt des Pylons">
<r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
<y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
<h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
</SurfaceRefPoint>
<SurfaceParameters Desc="Parametric description of pylon geometry">
<SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
<SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
<SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
<SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
<SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
</SurfaceParameters>
</Pylon>
<Pylon Desc="Beschreibung des Pylons" ID="LeftFuselagePylon">
<SurfaceRefPoint Desc="Referenzpunkt des Pylons">
<r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
<y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
<h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
</SurfaceRefPoint>
<SurfaceParameters Desc="Parametric description of pylon geometry">
<SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
<SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
<SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
<SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
<SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
<InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
<OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
<l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
<l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
<s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
<epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
<nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
<phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
</SurfaceSegment>
</SurfaceParameters>
</Pylon>
<Gear Desc="Beschreibung des Bugfahrwerks" ID="NoseGear">
<GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
<r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">3.480695762</r_Gear>
<y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear>
<h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.978883883</h_Gear>
</GearRefPoint>
<WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
<r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">3.480695762</r_Wheelgroup>
<y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup>
<h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-5.04556249</h_Wheelgroup>
</WheelGroupRefPoint>
<StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.127127</StrutDiameter>
<Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable>
<HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
<x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
<y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
<z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
</HingeAxis>
<RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">90</RetractionAngle>
<Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
<Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.3911791258</Wheeltrack>
<NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes>
<NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis>
<Wheel Desc="Beschreibung des Rades">
<TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0.6858</TireDiameter>
<TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.19558</TireWidth>
<RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.3429</RimDiameter>
</Wheel>
</Gear>
<Gear Desc="Beschreibung des aeusseren, rechten Hauptfahrwerks" ID="OuterRightMainGear">
<GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
<r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.84441297</r_Gear>
<y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">4.257464797</y_Gear>
<h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.313513579</h_Gear>
</GearRefPoint>
<WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
<r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.80664751</r_Wheelgroup>
<y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">4.257464797</y_Wheelgroup>
<h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.80426249</h_Wheelgroup>
</WheelGroupRefPoint>
<StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.32385</StrutDiameter>
<Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable>
<HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
<x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
<y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
<z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
</HingeAxis>
<RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">-90</RetractionAngle>
<Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
<Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.8636932256</Wheeltrack>
<NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes>
<NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis>
<Wheel Desc="Beschreibung des Rades">
<TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">1.1684</TireDiameter>
<TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.4318</TireWidth>
<RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.5842</RimDiameter>
</Wheel>
</Gear>
<Gear Desc="Beschreibung des aeusseren, linken Hauptfahrwerks" ID="OuterLeftMainGear">
<GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
<r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.84441297</r_Gear>
<y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-4.257464797</y_Gear>
<h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.313513579</h_Gear>
</GearRefPoint>
<WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
<r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.80664751</r_Wheelgroup>
<y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-4.257464797</y_Wheelgroup>
<h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.80426249</h_Wheelgroup>
</WheelGroupRefPoint>
<StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.32385</StrutDiameter>
<Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable>
<HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
<x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
<y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
<z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
</HingeAxis>
<RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">90</RetractionAngle>
<Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
<Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.8636932256</Wheeltrack>
<NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes>
<NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis>
<Wheel Desc="Beschreibung des Rades">
<TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">1.1684</TireDiameter>
<TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.4318</TireWidth>
<RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.5842</RimDiameter>
</Wheel>
</Gear>
<Gear Desc="Beschreibung des inneren, rechten Hauptfahrwerks" ID="InnerRightMainGear">
<GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
<r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Gear>
<y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear>
<h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Gear>
</GearRefPoint>
<WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
<r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Wheelgroup>
<y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup>
<h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Wheelgroup>
</WheelGroupRefPoint>
<StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0</StrutDiameter>
<Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">0</Retractable>
<HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
<x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
<y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
<z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
</HingeAxis>
<RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">0</RetractionAngle>
<Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
<Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0</Wheeltrack>
<NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">0</NumberOfAxes>
<NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">0</NumberOfWheelsPerAxis>
<Wheel Desc="Beschreibung des Rades">
<TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0</TireDiameter>
<TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0</TireWidth>
<RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0</RimDiameter>
</Wheel>
</Gear>
<Gear Desc="Beschreibung des inneren, linken Hauptfahrwerks" ID="InnerLeftMainGear">
<GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
<r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Gear>
<y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear>
<h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Gear>
</GearRefPoint>
<WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
<r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Wheelgroup>
<y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup>
<h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Wheelgroup>
</WheelGroupRefPoint>
<StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0</StrutDiameter>
<Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">0</Retractable>
<HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
<x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
<y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
<z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
</HingeAxis>
<RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">0</RetractionAngle>
<Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
<Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0</Wheeltrack>
<NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">0</NumberOfAxes>
<NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">0</NumberOfWheelsPerAxis>
<Wheel Desc="Beschreibung des Rades">
<TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0</TireDiameter>
<TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0</TireWidth>
<RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0</RimDiameter>
</Wheel>
</Gear>
</Geometry>
<Structure Desc="Strukturdaten"></Structure>
<Accommodation Desc="Kabineneinrichtung">
<PassengersTotal Desc="Gesamtanzahl der Sitzplaetze" ToolLevel="1">150</PassengersTotal>
<FlightCrew Desc="Anzahl Cockpitbesatzung" ToolLevel="1">2</FlightCrew>
<CabinCrew Desc="Anzahl Flugbegleiter" ToolLevel="1">4</CabinCrew>
<Seats Desc="Description of seats">
<NoOfSeatTypes Desc="Anzahl der Sitzklassen" ToolLevel="1">2</NoOfSeatTypes>
<seat Desc="Description of seat" ID="1">
<seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">economy</seatClassType>
<noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">4</noOfSeatConfigurations>
<seatConfiguration Desc="Description of SeatConfiguration" ID="1">
<mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">9</mass>
<noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
</seatConfiguration>
<seatConfiguration Desc="Description of SeatConfiguration" ID="2">
<mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">14</mass>
<noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
</seatConfiguration>
<seatConfiguration Desc="Description of SeatConfiguration" ID="3">
<mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">19.5</mass>
<noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats>
</seatConfiguration>
<seatConfiguration Desc="Description of SeatConfiguration" ID="4">
<mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">25</mass>
<noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">4</noOfSeats>
</seatConfiguration>
<IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">0</IFE>
<massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE>
</seat>
<seat Desc="Description of seat" ID="2">
<seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">business</seatClassType>
<noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">3</noOfSeatConfigurations>
<seatConfiguration Desc="Description of SeatConfiguration" ID="1">
<mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">27.2</mass>
<noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
</seatConfiguration>
<seatConfiguration Desc="Description of SeatConfiguration" ID="2">
<mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">35.1</mass>
<noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
</seatConfiguration>
<seatConfiguration Desc="Description of SeatConfiguration" ID="3">
<mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">43</mass>
<noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats>
</seatConfiguration>
<seatConfiguration Desc="Description of SeatConfiguration" ID="4">
<mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">25</mass>
<noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">4</noOfSeats>
</seatConfiguration>
<IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">1</IFE>
<massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE>
</seat>
</Seats>
<Galleys Desc="Description of galleys">
<NoOfGalleyTypes Desc="Anzahl verwendeter Kuechen Typen" ToolLevel="1">2</NoOfGalleyTypes>
<Gal Desc="Description of galley" ID="1">
<nameGalley Desc="Name of galley" ToolLevel="1">large</nameGalley>
<NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">1</NumberOfGalleys>
<mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">226.8</mass>
<power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">14418</power>
</Gal>
<Gal Desc="Description of galley" ID="2">
<nameGalley Desc="Name of galley" ToolLevel="1">small</nameGalley>
<NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">1</NumberOfGalleys>
<mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">61.24</mass>
<power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">3887</power>
</Gal>
</Galleys>
<Lavatories Desc="Description of lavatories">
<NoOfLavatoryTypes Desc="Anzahl verwendeter Lavatorie-Typen" ToolLevel="1">1</NoOfLavatoryTypes>
<Lav Desc="Description of lavatory" ID="1">
<nameLavatory Desc="Name of lavatory" ToolLevel="1">standard_lavatory</nameLavatory>
<NumberOfLavatories Desc="Gesamtzahl der verwendeten Lavatories dieses Typs" ToolLevel="1">3</NumberOfLavatories>
<mass Desc="Masse einer Lavatoryeinheit" ToolLevel="1" Unit="kg">96.67</mass>
</Lav>
</Lavatories>
<Cabin Desc="Beschreibung der Kabine">
<V_AirConditioned Desc="Klimatisiertes Kabinenvolumen gesamt" ToolLevel="1" Unit="m3">186.1462316</V_AirConditioned>
<CabinDecks Desc="Anzahl Kabinendecks" ToolLevel="1">1</CabinDecks>
<CabinDeck Desc="Parameter eines Kabinendecks" ID="1">
<A_CabinDeck Desc="Flaeche des Kabinendecks" ToolLevel="1" Unit="m2">97.50130651</A_CabinDeck>
<h_CabinDeck Desc="maximale Kabinenhoehe" ToolLevel="1" Unit="m">2.13</h_CabinDeck>
<w_CabinDeck Desc="maximale Kabinenbreite" ToolLevel="1" Unit="m">3.63012573</w_CabinDeck>
<l_CabinDeck Desc="Kabinenlaenge ohne Flight-Deck" ToolLevel="1" Unit="m">26.85893376</l_CabinDeck>
<V_CabinDeck Desc="Kabinenvolumen" ToolLevel="1" Unit="m3">184.2960557</V_CabinDeck>
<PAX_CabinDeck Desc="Sitzplaetze des Kabinendecks" ToolLevel="1">150</PAX_CabinDeck>
<Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck" ToolLevel="1">2</Classes>
<Class Desc="Definition der Klasse" ID="1">
<x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">5.983021821</x_center>
</Class>
<Class Desc="Definition der Klasse" ID="2">
<x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">19.4124887</x_center>
</Class>
</CabinDeck>
</Cabin>
<Cargo Desc="Beschreibung des Frachtraums">
<V_Cargo Desc="Frachtvolumen gesamt" ToolLevel="1" Unit="m3">35.92426606</V_Cargo>
<CargoDecks Desc="Anzahl Frachtdecks" ToolLevel="1">1</CargoDecks>
<CargoDeck Desc="Parameter eines Frachtdecks" ID="1">
<A_CargoDeck Desc="Flaeche des Frachtdecks" ToolLevel="1" Unit="m2">56.63668783</A_CargoDeck>
<h_CargoDeck Desc="maximale Deckhoehe" ToolLevel="1" Unit="m">1.14</h_CargoDeck>
<w_CargoDeck Desc="maximale Deckbreite" ToolLevel="1" Unit="m">3.280233538</w_CargoDeck>
<l_CargoDeck Desc="Decklaenge" ToolLevel="1" Unit="m">17.26605352</l_CargoDeck>
<V_CargoDeck Desc="Deckvolumen" ToolLevel="1" Unit="m3">36.40649695</V_CargoDeck>
<V_BulkCargo Desc="Freies Frachtvolumen fuer Bulk-Cargo" ToolLevel="1" Unit="m3">12.7695477</V_BulkCargo>
<Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck" ToolLevel="1">2</Compartments>
<Compartment Desc="Definition des Compartments" ID="1">
<Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">4.84</Length>
<x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">6.045</x_center>
</Compartment>
<Compartment Desc="Definition des Compartments" ID="2">
<Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">6.37</Length>
<x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">18.82863715</x_center>
</Compartment>
</CargoDeck>
</Cargo>
</Accommodation>
<Propulsion Desc="Angabe der verwendeten Engine Types (nicht jede einzelne Engine)">
<NumberOfEngineTypes Desc="Anzahl verschiedener Triebwerkstypen" ToolLevel="1">0</NumberOfEngineTypes>
<Engine Desc="Triebwerks-/Motortyp" ID="1">
<TypeOfEngine Desc="Triebwerkstyp z.Zt. Jet oder Prop" ToolLevel="1" Unit="-">jet</TypeOfEngine>
<EngineModel Desc="Triebwerksmodell fuer Gummimotor" ToolLevel="1" Unit="-">V2527-A5</EngineModel>
<NumberOfEngines Desc="Anzahl der Triebwerke - notwendig?" ToolLevel="1">2</NumberOfEngines>
<ScaleEngines Desc="Skalierungsfaktor fuer das Triebwerksmodell i.S.e. Gummimotors" ToolLevel="1" Unit="-">1.168175939</ScaleEngines>
<ScaleFuelFlow Desc="Skalierungsfaktor fuer den Fuel Flow" ToolLevel="1" Unit="-">1</ScaleFuelFlow>
<EngineDataFile Desc="Name der Triebewerksdatei (enthaelt Geometriedaten und Decks)" ToolLevel="1" Unit="-">engineData\V2527-A5\V2527-A5.xml</EngineDataFile>
<JetEngineData Desc="Jet spezifische Triebwerksdaten">
<SeaLevelStaticThrust Desc="Flat-Rated Standschub" ToolLevel="1" Unit="kN">128.8646365</SeaLevelStaticThrust>
<FanDiameter Desc="Durchmesser des Fans" ToolLevel="1" Unit="m">1.743365695</FanDiameter>
</JetEngineData>
<TurbopropEngineData Desc="Prop spezifische Triebwerksdaten">
<Prop Desc="Propellerdaten">
<PropDiameter Desc="Propellerdurchmesser" ToolLevel="1" Unit="m">0</PropDiameter>
<PropBlades Desc="Anzahl Propellerblaetter" ToolLevel="1">0</PropBlades>
<SegmentPointData ToolLevel="1">0</SegmentPointData>
<Pitch Desc="Variable oder Fix Pitch" ToolLevel="1">0</Pitch>
<Thickness Desc="Thickness of rotor disc " ToolLevel="1" Unit="m">0</Thickness>
</Prop>
<P_shp Desc="Triebwerkswellenleistung" ToolLevel="1" Unit="kW">0</P_shp>
</TurbopropEngineData>
<EngineDimensions Desc="Geometrische Abmasse des skalierten Triebwerks, Kerntriebwerk">
<w_Engine Desc="Breite des uninstallierten Triebwerks" ToolLevel="1" Unit="m">1.976823221</w_Engine>
<h_Engine Desc="Hoehe des uninstallierten Triebwerks" ToolLevel="1" Unit="m">2.289180745</h_Engine>
<l_Engine Desc="Gesamtlaenge des uninstallierten Triebwerks" ToolLevel="1" Unit="m">2.710701279</l_Engine>
</EngineDimensions>
<NacelleRescaling Desc="Parameter fuer Rescaling der Wing Nacelles" Matched="0">
<InnerNacelle>
<DeltaXPos Desc="Relative axiale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaXPos>
<RelYPos Desc="Relative spannweitige Position der Nacelle" ToolLevel="1" Unit="-">0</RelYPos>
<DeltaZPos Desc="Relative vertikale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaZPos>
<WidthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-breite" ToolLevel="1" Unit="-">0</WidthRatio>
<HeightRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-hoehe" ToolLevel="1" Unit="-">0</HeightRatio>
<LengthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-laenge" ToolLevel="1" Unit="-">0</LengthRatio>
</InnerNacelle>
<OuterNacelle>
<DeltaXPos Desc="Relative axiale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaXPos>
<RelYPos Desc="Relative spannweitige Position der Nacelle" ToolLevel="1" Unit="-">0</RelYPos>
<DeltaZPos Desc="Relative vertikale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaZPos>
<WidthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-breite" ToolLevel="1" Unit="-">0</WidthRatio>
<HeightRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-hoehe" ToolLevel="1" Unit="-">0</HeightRatio>
<LengthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-laenge" ToolLevel="1" Unit="-">0</LengthRatio>
</OuterNacelle>
</NacelleRescaling>
<ScaledPerformanceCharacteristics Desc="Leistungscharakteristik des (eines!) skalierten Triebwerks">
<EquivalentThrust Desc="1.25 * Max-Go-Around (Schub bei ISA+deltaISA(Requirements/DesignMission), SL, Ma0.25, N1 100 perc)" ToolLevel="1" Unit="kN">127.3858501</EquivalentThrust>
<MaximumTakeOff Desc="Maximale Startschubbedingung bei ISA+deltaISA(Requirements/DesignMission) und keinen Off-takes bei Altitude_ft=0.0 Mach=0.0">
<Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">128.8646365</Thrust>
<FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">1.316357232</FuelFlow>
<TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01021503857</TSFC>
<N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.9783203125</N1>
</MaximumTakeOff>
<MaximumGoAround Desc="Maximale Go-Around-Bedingung bei ISA+deltaISA(Requirements/DesignMission) und keinen Off-takes bei Altitude_ft=0.0, Mach=0.25">
<Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">101.9086801</Thrust>
<FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">1.329201509</FuelFlow>
<TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01304306471</TSFC>
<N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.9734765625</N1>
</MaximumGoAround>
<MaximumContinous Altitude_ft="35000" Desc="Maximales Schublimit ohne Zeitlimit bei ISA+deltaISA(Requirements/DesignMission) bei" Mach="0.8">
<MaxThrust Desc="Without Offtakes">
<Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">32.18450048</Thrust>
<FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.5460196217</FuelFlow>
<TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01696529738</TSFC>
<N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.981796875</N1>
</MaxThrust>
<BucketThrust Desc="Without Offtakes">
<Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">29.28223674</Thrust>
<FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.4959848906</FuelFlow>
<TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01693808075</TSFC>
<N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.950379375</N1>
</BucketThrust>
<BucketThrustOfftakes Desc="With Average Cruise Offtakes (s. Design Mission)">
<Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">29.28223674</Thrust>
<FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.5130623087</FuelFlow>
<TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01752128136</TSFC>
<N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.950379375</N1>
</BucketThrustOfftakes>
</MaximumContinous>
</ScaledPerformanceCharacteristics>
<UsedForNacelles Desc="Angabe der Nacelle IDs, in welche dieser Engine Type eingebaut wird">
<UsedForNumberOfEngines ToolLevel="1">0</UsedForNumberOfEngines>
<NacelleID ID="1" ToolLevel="1">0</NacelleID>
<NacelleID ID="2" ToolLevel="1">0</NacelleID>
<NacelleID ID="3" ToolLevel="1">0</NacelleID>
<NacelleID ID="4" ToolLevel="1">0</NacelleID>
</UsedForNacelles>
</Engine>
</Propulsion>
<Systems>
<FuelTank Desc="Tank system Parameters">
<CentreTanks Desc="No of centre tanks" ToolLevel="1">1</CentreTanks>
<CentreTank Desc="Centre tank description" ID="1">
<TankVolume Desc="Tank volume" ToolLevel="1" Unit="l">10541.14749</TankVolume>
</CentreTank>
<WingTanks Desc="No of wing tanks" ToolLevel="1">2</WingTanks>
<WingTank Desc="Wing tank description" ID="1">
<TankVolume Desc="Tank volume" ToolLevel="1" Unit="l">15416.66477</TankVolume>
</WingTank>
<WingTank Desc="Wing tank description" ID="2">
<TankVolume Desc="Tank volume" ToolLevel="1" Unit="l">15416.66477</TankVolume>
</WingTank>
<TrimTanks Desc="No of trim tanks" ToolLevel="1">0</TrimTanks>
<TrimTank Desc="Trim tank description" ID="1">
<TankVolume Desc="Tank volume" ToolLevel="1" Unit="l">0</TankVolume>
</TrimTank>
<FuselageTanks Desc="No of fuselage tanks" ToolLevel="1">0</FuselageTanks>
<FuselageTank Desc="Fuselage tank description" ID="1">
<TankVolume Desc="Tank volume" ToolLevel="1" Unit="l">0</TankVolume>
</FuselageTank>
<TotalFuelVolume Desc="Total fuel volume of all tanks" ToolLevel="1" Unit="l">41374.47702</TotalFuelVolume>
</FuelTank>
<ATA21_EnvironmentalControlSystem>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">25.37098678</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">1.31382376</BleedAir>
</DesignPower>
<AirflowPerPax Desc="Konstanter Luftmassenstrom pro Passagier" ToolLevel="1" Unit="lbs/min">0.75</AirflowPerPax>
<Recirculation Desc="Prozentualer Anteil der Kabinenluft, die wieder verwendet wird (0.0 - 1.0)" ToolLevel="1" Unit="-">0.4</Recirculation>
</ATA21_EnvironmentalControlSystem>
<ATA22_AutoFlight>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
</DesignPower>
</ATA22_AutoFlight>
<ATA23_Communication>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
</DesignPower>
</ATA23_Communication>
<ATA24_ElectricSystem>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
</DesignPower>
</ATA24_ElectricSystem>
<ATA25_Furnishing>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">18.92</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
</DesignPower>
</ATA25_Furnishing>
<ATA26_FireProtection>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
</DesignPower>
</ATA26_FireProtection>
<ATA27_FlightControlSystem>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">93.56406668</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
</DesignPower>
</ATA27_FlightControlSystem>
<ATA28_FuelSystem>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">12.23167268</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
</DesignPower>
</ATA28_FuelSystem>
<ATA29_HydraulicSystem>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">7.451202472</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
</DesignPower>
<Pressure Desc="Nenn-Druck des Hydrauliksystems" ToolLevel="1" Unit="psi">3000</Pressure>
</ATA29_HydraulicSystem>
<ATA30_IceRainProtection>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">14.0269</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0.6613272863</BleedAir>
</DesignPower>
</ATA30_IceRainProtection>
<ATA31_Instrumentation>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
</DesignPower>
</ATA31_Instrumentation>
<ATA32_LandingGear>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">74.97503685</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
</DesignPower>
</ATA32_LandingGear>
<ATA33_Lights>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">7.884251516</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
</DesignPower>
</ATA33_Lights>
<ATA34_Navigation>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
</DesignPower>
</ATA34_Navigation>
<ATA35_Oxygen>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
</DesignPower>
</ATA35_Oxygen>
<ATA36_BleedAir>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0.1039553182</BleedAir>
</DesignPower>
</ATA36_BleedAir>
<ATA49_APU>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">-0</BleedAir>
</DesignPower>
</ATA49_APU>
<ATA70_PropulsionSystem>
<DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
<Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">-205.4781816</Electric>
<Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">-181.0078664</Hydraulic>
<BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">-2.188533015</BleedAir>
</DesignPower>
</ATA70_PropulsionSystem>
</Systems>
<Aerodynamics Desc="Aerodynamik">
<LoverD_Cruise Desc="Beste Gleitzahl L/D im Reiseflug fuer (Initial) Cruise Machzahl" ToolLevel="1" Unit="-">16.46037111</LoverD_Cruise>
<LiftCoefficients Desc="Auftriebsbeiwerte">
<C_L_design Desc="Design Auftriebsbeiwert" ToolLevel="1" Unit="-">0.5381848981</C_L_design>
<C_LmaxLanding Desc="Maximaler Auftriebsbeiwert Landekonfiguration" ToolLevel="1" Unit="-">2.916185004</C_LmaxLanding>
<C_LmaxT-O Desc="Maximaler Auftriebsbeiwert Startkonfiguration" ToolLevel="1" Unit="-">2.515329503</C_LmaxT-O>
<C_LoptimumCruise Desc="Auftriebsbeiwert bei bestem LoverD bei (Initial) Cruise Machzahl" ToolLevel="1" Unit="-">0.528</C_LoptimumCruise>
<C_L_opt_wing Desc="Auftriebsbeiwert bei bestem LoverD (Anteil Fluegel)" ToolLevel="1" Unit="-">0.5626638406</C_L_opt_wing>
<C_L_opt_stab Desc="Auftriebsbeiwert bei bestem LoverD (Anteil HLW)" ToolLevel="1" Unit="-">-0.03466354382</C_L_opt_stab>
<C_LgroundRoll Desc="lift coefficient on ground for ground roll calculation" ToolLevel="1" Unit="-">0.4</C_LgroundRoll>
</LiftCoefficients>
<DragCoefficients Desc="Widerstandsbeiwerte (bei bestem L/D im Cruise, s.o.)">
<C_D_total Desc="Widerstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.03207704106</C_D_total>
<C_D_ind Desc="induzierter Widerstandsbeiwert" ToolLevel="1" Unit="-">0.009803808575</C_D_ind>
<C_D_visc Desc="Reibungswiderstandsbeiwerte" ToolLevel="1" Unit="-">
<C_D_visc_total Desc="Reibungswiderstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.01972511904</C_D_visc_total>
<C_D_visc_wing Desc="Reibungswiderstandsbeiwert Fluegel" ToolLevel="1" Unit="-">0.00660550988</C_D_visc_wing>
<C_D_visc_stab Desc="Reibungswiderstandsbeiwert HLW" ToolLevel="1" Unit="-">0.001454379701</C_D_visc_stab>
<C_D_visc_fin Desc="Reibungswiderstandsbeiwert SLW" ToolLevel="1" Unit="-">0.001569261547</C_D_visc_fin>
<C_D_visc_fus Desc="Reibungswiderstandsbeiwert Rumpf" ToolLevel="1" Unit="-">0.006412233533</C_D_visc_fus>
<C_D_visc_nac Desc="Reibungswiderstandsbeiwert Nacelle" ToolLevel="1" Unit="-">0.001743616971</C_D_visc_nac>
<C_D_visc_misc Desc="Reibungswiderstandsbeiwert weitere" ToolLevel="1" Unit="-">0.001940117406</C_D_visc_misc>
</C_D_visc>
<C_D_wave Desc="Wellenwiderstandsbeiwerte" ToolLevel="1" Unit="-">
<C_D_wave_total Desc="Wellenwiderstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.002548113448</C_D_wave_total>
<C_D_wave_wing Desc="Wellenwiderstandsbeiwert Fluegel" ToolLevel="1" Unit="-">0.002547491352</C_D_wave_wing>
<C_D_wave_stab Desc="Wellenwiderstandsbeiwert HLW" ToolLevel="1" Unit="-">6.220952302e-07</C_D_wave_stab>
</C_D_wave>
<EoW_DragFactor Desc="Drag factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_DragFactor>
</DragCoefficients>
<MomentCoefficients Desc="Momentenbeiwerte (getrimmt, bei bestem L/D im Cruise, s.o.)">
<C_M_total Desc="Momentenbeiwert bei optimum Cruise" ToolLevel="1" Unit="-">1.138318599e-05</C_M_total>
</MomentCoefficients>
<Polar Desc="Flugzeugpolare">
<PolarFile Desc="Dateiname der Flugzeugpolare" ToolLevel="1" Unit="-">aeroData\CSR-02_polar.xml</PolarFile>
<Configurations Desc="Anzahl der aerodynamischen Konfigurationen in der Polarendatei" ToolLevel="1">7</Configurations>
<Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="1" ToolLevel="1" Type="Cruise">Clean</Configuration>
<Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="2" ToolLevel="1" Type="Departure">TakeOff</Configuration>
<Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="3" ToolLevel="1" Type="Departure">TakeOffLGRetracted</Configuration>
<Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="4" ToolLevel="1" Type="Departure">Climb</Configuration>
<Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="5" ToolLevel="1" Type="Approach">Approach</Configuration>
<Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="6" ToolLevel="1" Type="Approach">ApproachLG</Configuration>
<Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="7" ToolLevel="1" Type="Approach">Landing</Configuration>
</Polar>
<ReferenceValues Desc="Aerodynamische Bezugsgroessen">
<b Desc="Total wing span" ToolLevel="1" Unit="m">34.66122714</b>
<MAC Desc="Mean aerodynamic chord" ToolLevel="1" Unit="m">4.402512853</MAC>
<S_ref Desc="Wing reference area" ToolLevel="1" Unit="m2">126.463228</S_ref>
</ReferenceValues>
<MaxSpoilerFactor Desc="Faktor zur max. Widerstandserhoehung durch Spoiler" ToolLevel="1" Unit="-">2.5</MaxSpoilerFactor>
</Aerodynamics>
<StabilityAndControlCharacteristics Desc="Flugmechanik, Stabilitaet und Steuerbarkeit">
<Stabiliser>
<VolumeCoefficient Desc="berechneter Volumenkoeffizient" Matched="1" ToolLevel="1" Unit="-">1.017690098</VolumeCoefficient>
<S_ref Desc="Stabiliser reference area" ToolLevel="1" Unit="m2">32.94519006</S_ref>
</Stabiliser>
<VerticalTail>
<VolumeCoefficient Desc="berechneter Volumenkoeffizient" Matched="1" ToolLevel="1" Unit="-">0.09489408521</VolumeCoefficient>
<S_ref Desc="Fin reference area" ToolLevel="1" Unit="m2">25.44285876</S_ref>
</VerticalTail>
</StabilityAndControlCharacteristics>
<Performance Desc="Flugleistungen">
<Range Desc="Reichweiten">
<Range_maxPayloadatMTOM Desc="Reichweite bei maximaler Nutzlast und Betankung bis zum MTOM-Limit" ToolLevel="2" Unit="km">3246.670783</Range_maxPayloadatMTOM>
<Range_maxFuelatMTOM Desc="Reichweite bei vollen Tanks und Nutzlast bis zum MTOM-Limit" ToolLevel="2" Unit="km">10458.2771</Range_maxFuelatMTOM>
<Payload_maxFuelatMTOM Desc="Payload bei vollen Tanks und Nutzlast bis zum MTOM-Limit" ToolLevel="2" Unit="kg">4360.32531</Payload_maxFuelatMTOM>
<Range_maxFuelEmpty Desc="Ueberfuehrungsreichweite, leer mit vollen Tanks" ToolLevel="2" Unit="km">10709.69495</Range_maxFuelEmpty>
</Range>
<Speed Desc="Fluggeschwindigkeiten">
<M_initialCruise Desc="Cruisemachzahl" ToolLevel="3" Unit="-">0.78</M_initialCruise>
<M_maxOperating Desc="Max Operating Cruise Machzahl" ToolLevel="2" Unit="-">0.82</M_maxOperating>
<V_maxOperating Desc="Max Operating Speed (Maximale Staudruckgeschwindigkeit CAS/IAS)" ToolLevel="2" Unit="KCAS">350</V_maxOperating>
<M_Dive Desc="Diving Mach Number" ToolLevel="2" Unit="-">0.902</M_Dive>
<V_Dive Desc="Diving Speed" ToolLevel="2" Unit="KCAS">385</V_Dive>
<V_s1g Desc="1-g Stalling Speed" ToolLevel="2" Unit="KCAS">154.8031322</V_s1g>
</Speed>
<Altitudes Desc="Flughoehen">
<h_initialCruise Desc="Reiseflughoehe" ToolLevel="3" Unit="m">10058.4</h_initialCruise>
<h_maxCertified Desc="maximal zugelassene Flughoehe (s. TLAR)" ToolLevel="3" Unit="m">11734.8</h_maxCertified>
<h_maxOperating Desc="Dienstgipfelhoehe (100 ft/min Steigkriterium)" ToolLevel="3" Unit="m">11713.23959</h_maxOperating>
<h_maxCeiling Desc="Maximale Flughoehe (50 ft/min Steigkriterium) bei MTOM" ToolLevel="3" Unit="m">11763.23474</h_maxCeiling>
<h_maxOEI Desc="Maximale Flughoehe (100 ft/min Steigkriterium) bei einem Triebwerksausfall und bei MTOM" ToolLevel="3" Unit="m">6608.028951</h_maxOEI>
</Altitudes>
<Climb Desc="Climb Performance">
<TTC_Design Desc="Time needed to climb from 1500ft to ICA (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="min">16.15883289</TTC_Design>
<TTC_ISA Desc="Time needed to climb from 1500ft to ICA (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="min">16.15883289</TTC_ISA>
<Time_to_1500ft_ISA Desc="Time needed to climb from BR to 1500ft (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="min">1.251683745</Time_to_1500ft_ISA>
<Time_to_ICA_ISA Desc="Time needed to climb from BR to ICA (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="min">17.41051663</Time_to_ICA_ISA>
<Range_to_ICA_ISA Desc="Range needed to climb from BR to ICA (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="NM">101.9061674</Range_to_ICA_ISA>
<Fuel_to_ICA_ISA Desc="Fuel mass needed to climb from BR to ICA (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="kg">1715.660845</Fuel_to_ICA_ISA>
</Climb>
<TakeOff Desc="Start Performance">
<TakeOffDistance_Normal Desc="Takeoff distance at Sea Level for MTOM and (ISA + deltaISA)-Conditions(calculated by missionAnalysis using missionDesign.xml settings)" ToolLevel="3" Unit="m">660.3942437</TakeOffDistance_Normal>
<TakeOffDistance_Normal_Safety Desc="Takeoff distance at Sea Level for MTOM and ISA+deltaISA(Requirements/DesignMission) (incl. 15 percent safety margin; estimated by calculatePerformance)" ToolLevel="2" Unit="m">1314.175463</TakeOffDistance_Normal_Safety>
<BFL Desc="Design takeoff distance - Balanced Field Length at Sea Level with MTOM and ISA+deltaISA(Requirements/DesignMission)-Conditions" ToolLevel="2" Unit="m">0</BFL>
<TimeToScreenHeight Desc="Time until reaching screen height (35ft) at Sea Level with MTOM and ISA+deltaISA(Requirements/DesignMission)-Conditions" ToolLevel="2" Unit="s">28.99214318</TimeToScreenHeight>
<V_LOF Desc="Lift-off speed at Sea Level for MTOM and ISA+deltaISA(Requirements/DesignMission)-Conditions" ToolLevel="2" Unit="KCAS">126.3711884</V_LOF>
<V_1 Desc="Decision Speed at Sea Level for MTOM and ISA+deltaISA(Requirements/DesignMission)-Conditions" ToolLevel="2" Unit="KCAS">0</V_1>
<V_2 Desc="Speed at screen height (35 ft)" ToolLevel="2" Unit="KCAS">126.3711884</V_2>
<V_FTO Desc="Speed at final takeoff segment (1500 ft)" ToolLevel="2" Unit="KCAS">202.4392823</V_FTO>
<ScdSegmentClimbGradient Desc="Climb gradient in second takeoff segment" ToolLevel="2" Unit="%">2.416614712</ScdSegmentClimbGradient>
<FinalSegmentClimbGradient Desc="Climb gradient in final takeoff segment" ToolLevel="2" Unit="%">2.416614712</FinalSegmentClimbGradient>
</TakeOff>
<Landing>
<LandingDistance Desc="Landing distance at Sea Level for MLM and (ISA + deltaISA)-Conditions(calculated by missionAnalysis using missionDesign.xml settings)" ToolLevel="3" Unit="m">1373.253939</LandingDistance>
<NeededRunwayLength Desc="Needed runway length at Sea Level with MLM and ISA+deltaISA(Requirements/DesignMission)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6)" ToolLevel="2" Unit="m">1680.105692</NeededRunwayLength>
<V_Approach Desc="Final Approach Speed" ToolLevel="2" Unit="KCAS">128.6850003</V_Approach>
</Landing>
<MissionAnalysis Desc="Missionsanalyse">
<DesignMission Desc="Parameter der Design-Mission">
<MissionFile Desc="Dateiname der Missionsdatei" ToolLevel="1" Unit="-">missionData\missionDesign.xml</MissionFile>
<CruiseSteps Desc="Anzahl der Hoehenschritte im Reiseflug-Missionsprofil" ToolLevel="3">2</CruiseSteps>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="1">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">0.5009643041</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">330.0000005</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="2">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">1</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">350.0000005</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="3">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="4">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="5">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="6">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="7">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="8">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="9">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="10">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="11">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="12">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="13">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="14">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="15">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<Missionfuel Desc="Getankter Kraftstoff (Tripfuel + Reserve Fuel + TaxifuelTakeoff)" ToolLevel="3" Unit="kg">19940.80556</Missionfuel>
<Tripfuel Desc="Tripfuel (Fuel burned from takeoff to landing)" ToolLevel="3" Unit="kg">16588.93118</Tripfuel>
<TaxifuelTakeoff Desc="Taxifuel vor dem Start" ToolLevel="3" Unit="kg">101.5157969</TaxifuelTakeoff>
<TaxifuelLdg Desc="Taxifuel nach der Landung" ToolLevel="3" Unit="kg">56.39766495</TaxifuelLdg>
<Blocktime Desc="Blocktime" ToolLevel="3" Unit="h">5.94079849</Blocktime>
<Flighttime Desc="Flugzeit ohne taxi" ToolLevel="3" Unit="h">5.707465156</Flighttime>
<Range Desc="Range" ToolLevel="3" Unit="NM">2500.496213</Range>
<TOM Desc="geflogenes Take Off Mass" ToolLevel="3" Unit="kg">79148.59668</TOM>
<Payload Desc="geflogene Payload" ToolLevel="3" Unit="kg">17000</Payload>
<NumberOfPAX Desc="Anzahl Passagiere" ToolLevel="3" Unit="-">150</NumberOfPAX>
<CargoMass Desc="Frachtmasse" ToolLevel="3" Unit="kg">3392</CargoMass>
<TakeOffEngineDerate Desc="Engine Derate (AMTC,eng); reduced takeoff-thrust" ToolLevel="3" Unit="-">1</TakeOffEngineDerate>
<Offtakes>
<AverageCruiseOfftakes Desc="Durschnittliche Entnahmen fuer Cruise-Modes Cruise und ChangeFL">
<ShaftPowerTotal Desc="Gesamte Wellenleistungsentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kW">103.3245182</ShaftPowerTotal>
<BleedAirTotal Desc="Gesamte Zapfluftentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kg/s">0.8796612188</BleedAirTotal>
</AverageCruiseOfftakes>
</Offtakes>
<LiftCoefficientsCruise Desc="Erflogene Auftriebsbeiwerte im Reiseflug">
<CL_avg Desc="Arithm. Mittelwert ueber gesamten Reiseflug" ToolLevel="3" Unit="-">0.5101767772</CL_avg>
<CL_min Desc="Min. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4831782814</CL_min>
<CL_max Desc="Max. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.5667676169</CL_max>
</LiftCoefficientsCruise>
<MassesCruise Desc="Gesamtflugzeugmassen waehrend des Reiseflugs">
<Mass_TOC Desc="Gesamtflugzeugmasse am Top-of-Climb-Punkt (ICA)" ToolLevel="3" Unit="kg">77451.03811</Mass_TOC>
<Mass_TOD Desc="Gesamtflugzeugmasse am Top-of-Descent-Punkt" ToolLevel="3" Unit="kg">63267.90838</Mass_TOD>
</MassesCruise>
</DesignMission>
<StudyMission Desc="Parameter der Study-Mission">
<MissionFile Desc="Dateiname der Missionsdatei" ToolLevel="1" Unit="-">missionData\missionStudy.xml</MissionFile>
<CruiseSteps Desc="Anzahl der Hoehenschritte im Reiseflug-Missionsprofil" ToolLevel="3">1</CruiseSteps>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="1">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">1</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">350.0000005</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="2">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="3">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="4">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="5">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="6">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="7">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="8">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="9">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="10">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="11">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="12">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="13">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="14">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="15">
<RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
<FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
</CruiseStep>
<Missionfuel Desc="Getankter Kraftstoff (Tripfuel + Reserve Fuel + TaxifuelTakeoff)" ToolLevel="3" Unit="kg">6746.530829</Missionfuel>
<Tripfuel Desc="Tripfuel (Fuel burned from takeoff to landing)" ToolLevel="3" Unit="kg">3818.187572</Tripfuel>
<TaxifuelTakeoff Desc="Taxifuel vor dem Start" ToolLevel="3" Unit="kg">101.5158315</TaxifuelTakeoff>
<TaxifuelLdg Desc="Taxifuel nach der Landung" ToolLevel="3" Unit="kg">56.39768417</TaxifuelLdg>
<Blocktime Desc="Blocktime" ToolLevel="3" Unit="h">1.499139745</Blocktime>
<Flighttime Desc="Flugzeit ohne taxi" ToolLevel="3" Unit="h">1.265806411</Flighttime>
<Range Desc="Range" ToolLevel="3" Unit="NM">500.6435758</Range>
<TOM Desc="geflogenes Take Off Mass" ToolLevel="3" Unit="kg">62562.32191</TOM>
<Payload Desc="geflogene Payload" ToolLevel="3" Unit="kg">13608</Payload>
<NumberOfPAX Desc="Anzahl Passagiere" ToolLevel="3" Unit="-">150</NumberOfPAX>
<CargoMass Desc="Frachtmasse" ToolLevel="3" Unit="kg">0</CargoMass>
<TakeOffEngineDerate Desc="Engine Derate (AMTC,eng); reduced takeoff-thrust" ToolLevel="3" Unit="-">1</TakeOffEngineDerate>
<Offtakes>
<AverageCruiseOfftakes Desc="Durschnittliche Entnahmen fuer Cruise-Modes Cruise und ChangeFL">
<ShaftPowerTotal Desc="Gesamte Wellenleistungsentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kW">102.8677337</ShaftPowerTotal>
<BleedAirTotal Desc="Gesamte Zapfluftentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kg/s">0.8796612188</BleedAirTotal>
</AverageCruiseOfftakes>
</Offtakes>
<LiftCoefficientsCruise Desc="Erflogene Auftriebsbeiwerte im Reiseflug">
<CL_avg Desc="Arithm. Mittelwert ueber gesamten Reiseflug" ToolLevel="3" Unit="-">0.4609914236</CL_avg>
<CL_min Desc="Min. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4538594196</CL_min>
<CL_max Desc="Max. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4925634903</CL_max>
</LiftCoefficientsCruise>
<MassesCruise Desc="Gesamtflugzeugmassen waehrend des Reiseflugs">
<Mass_TOC Desc="Gesamtflugzeugmasse am Top-of-Climb-Punkt (ICA)" ToolLevel="3" Unit="kg">61280.43659</Mass_TOC>
<Mass_TOD Desc="Gesamtflugzeugmasse am Top-of-Descent-Punkt" ToolLevel="3" Unit="kg">59428.93455</Mass_TOD>
</MassesCruise>
</StudyMission>
</MissionAnalysis>
<RequirementsChecks>
<MissionFile Desc="Dateiname der Missionsdatei" OfftakesWritten="1" ToolLevel="1" Unit="-">missionData\missionReq.xml</MissionFile>
<TLARs>
<TOFL_Design Checked="1" ToolLevel="2">1</TOFL_Design>
<LDN_Design Checked="1" ToolLevel="2">1</LDN_Design>
<V_ApproachSpeed_Design Checked="1" ToolLevel="2">1</V_ApproachSpeed_Design>
<h_initialCruise_Design Checked="1" ToolLevel="3">1</h_initialCruise_Design>
<h_maxOperating Checked="1" ToolLevel="3">1</h_maxOperating>
<h_maxOEI Checked="1" ToolLevel="3">1</h_maxOEI>
<M_initialCruise_Design Checked="1" ToolLevel="3">1</M_initialCruise_Design>
<TTC_Design Checked="1" ToolLevel="3">1</TTC_Design>
</TLARs>
<Certification>
<climbGradientSecondTOSegment Checked="1" ToolLevel="2">1</climbGradientSecondTOSegment>
<climbGradientFinalTOSegment Checked="1" ToolLevel="2">1</climbGradientFinalTOSegment>
<climbGradientApproachOEI Checked="1" ToolLevel="2">1</climbGradientApproachOEI>
<climbGradientApproachAEO Checked="1" ToolLevel="2">1</climbGradientApproachAEO>
</Certification>
</RequirementsChecks>
</Performance>
<MonetaryValues Desc="Kosten und Preise">
<MonetaryScenario>
<AirframeEngineeringHours Desc="Anzahl der Arbeitsstunden in der FZ-Entwicklung" ToolLevel="1" Unit="h">0</AirframeEngineeringHours>
<ProductionVolume Desc="Anzahl produzierter Flugzeuge je Programm" ToolLevel="1">0</ProductionVolume>
</MonetaryScenario>
<Earnings Desc="Herstellergewinn pro verkauftem Flugzeug" ToolLevel="1" Unit="$">0</Earnings>
<NPV Desc="Net Present Value (Kapitalwert) fuer Flugzeugprogramm bei Verkauf des gesamten ProductionVolume" ToolLevel="1" Unit="Mio.$">0</NPV>
<Prices Desc="Preise">
<PriceAirplane Desc="airplane price (for the whole plane); for the insurance and for the Simple_deprecition in DOC-Tool" ToolLevel="1" Unit="$">0</PriceAirplane>
<DiscountRate Desc="discount rate on airplane lst price granted airlines" ToolLevel="1" Unit="-">0</DiscountRate>
</Prices>
<LCC Desc="Life Cycle Costs">
<NonRecurringCosts Desc="Non-Recurring Costs fuer gesamtes Flugzeugprogramm">
<NRCTotal Desc="Non Recurring Costs" ToolLevel="1" Unit="$">0</NRCTotal>
<NRCComponents>
<AirframeEngAndDesign Desc="Costs for Airframe Engineering and Design" ToolLevel="1" Unit="$">0</AirframeEngAndDesign>
<DevSupportAndTesting Desc="Costs for Development Support and Testing" ToolLevel="1" Unit="$">0</DevSupportAndTesting>
<FlightTestAC>
<FlightTestACTotal Desc="Costs for Flight Test Aircraft" ToolLevel="1" Unit="$">0</FlightTestACTotal>
<FlightTestACComponents>
<EngineAndAvionics Desc="Costs for Engines and Avionics" ToolLevel="1" Unit="$">0</EngineAndAvionics>
<LaborManufacturing Desc="Costs for Manufacturing Labor" ToolLevel="1" Unit="$">0</LaborManufacturing>
<MaterialManufacturing Desc="Costs for Manufacturing Material" ToolLevel="1" Unit="$">0</MaterialManufacturing>
<Tooling Desc="Costs for Tooling" ToolLevel="1" Unit="$">0</Tooling>
<QualityControl Desc="Costs for Quality Control" ToolLevel="1" Unit="$">0</QualityControl>
</FlightTestACComponents>
</FlightTestAC>
<FlightTestOp Desc="Costs for Flight Test Operations" ToolLevel="1" Unit="$">0</FlightTestOp>
<Facilities Desc="Costs for Test and Simulation Facilities" ToolLevel="1" Unit="$">0</Facilities>
</NRCComponents>
</NonRecurringCosts>
<RecurringCosts Desc="Recurring Costs">
<RCTotal Desc="Recurring Costs" ToolLevel="1" Unit="$">0</RCTotal>
<RCComponents>
<Wing Desc="Costs for Wing" ToolLevel="1" Unit="$">0</Wing>
<Fuselage Desc="Costs for Fuselage" ToolLevel="1" Unit="$">0</Fuselage>
<Empennage Desc="Costs for Empennage" ToolLevel="1" Unit="$">0</Empennage>
<LandingGear Desc="Costs for Landing Gear" ToolLevel="1" Unit="$">0</LandingGear>
<Pylons Desc="Costs for Pylons" ToolLevel="1" Unit="$">0</Pylons>
<PowerUnit Desc="Costs for all installed engines with systems without pylons">
<PowerUnitTotal Desc="Costs for PowerUnit" ToolLevel="1" Unit="$">0</PowerUnitTotal>
<PowerUnitComponents>
<EquippedEngines Desc="Costs for Engines Dry and Other Systems" ToolLevel="1" Unit="$">0</EquippedEngines>
<Nacelles Desc="Costs for Nacelles" ToolLevel="1" Unit="$">0</Nacelles>
<BleedAirSystem Desc="Costs for BleedAirSystem (Airbus Chapter 21, ATA36)" ToolLevel="1" Unit="$">0</BleedAirSystem>
<FuelSystem Desc="Costs for Fuel System (Airbus Chapter 23, ATA28)" ToolLevel="1" Unit="$">0</FuelSystem>
</PowerUnitComponents>
</PowerUnit>
<Systems>
<SystemsTotal Desc="Costs for Systems" ToolLevel="1" Unit="$">0</SystemsTotal>
<SystemsComponents>
<APU Desc="Costs for APU (Airbus Chapter 30, ATA49)" ToolLevel="1" Unit="$">0</APU>
<HydraulicSystem Desc="Costs for Hydraulic System (Airbus Chapter 31 + 32,ATA29)" ToolLevel="1" Unit="$">0</HydraulicSystem>
<AirConditioning Desc="Costs for Air Conditioning (Airbus Chapter 33, ATA21)" ToolLevel="1" Unit="$">0</AirConditioning>
<DeIcing Desc="Costs for De-Icing (Airbus Chapter 34, ATA30)" ToolLevel="1" Unit="$">0</DeIcing>
<FireProtection Desc="Costs for Fire Protection (Airbus Chapter 35, ATA26)" ToolLevel="1" Unit="$">0</FireProtection>
<FlightControls Desc="Costs for Flight Controls (Airbus Chapter 36, ATA27)" ToolLevel="1" Unit="$">0</FlightControls>
<Instruments Desc="Costs for Instruments (Airbus Chapter 37, ATA31)" ToolLevel="1" Unit="$">0</Instruments>
<AutomaticFlightSystem Desc="Costs for Automatic Flight System (Airbus Chapter 38, ATA22)" ToolLevel="1" Unit="$">0</AutomaticFlightSystem>
<Navigation Desc="Costs for Navigation (Airbus Chapter 39, ATA34)" ToolLevel="1" Unit="$">0</Navigation>
<Communication Desc="Costs for Communication (Airbus Chapter 40, ATA23)" ToolLevel="1" Unit="$">0</Communication>
<ElectricalSystem Desc="Costs for Air Conditioning (Airbus Chapter 41+42, ATA24)" ToolLevel="1" Unit="$">0</ElectricalSystem>
</SystemsComponents>
</Systems>
<Furnishings>
<FurnishingsTotal Desc="Costs for Furnishings" ToolLevel="1" Unit="$">0</FurnishingsTotal>
<FurnishingsComponents>
<Furnishing Desc="Costs for Furnishings (Airbus Chapter 50, ATA25)" ToolLevel="1" Unit="$">0</Furnishing>
<FixedEmergencyOxygen Desc="Costs for Fixed Emergency Oxygen (Airbus Chapter 51, ATA35)" ToolLevel="1" Unit="$">0</FixedEmergencyOxygen>
<Lighting Desc="Costs for Lighting (Airbus Chapter 52, ATA33)" ToolLevel="1" Unit="$">0</Lighting>
<WaterInstallation Desc="Costs for Water Installation (Airbus Chapter 53, ATA38)" ToolLevel="1" Unit="$">0</WaterInstallation>
</FurnishingsComponents>
</Furnishings>
<OperatorsItems Desc="Costs for OperatorItems (Airbus Chapter 60+61)" ToolLevel="1" Unit="$">0</OperatorsItems>
<FinalAssembly Desc="Costs for FinalAssembly" ToolLevel="1" Unit="$">0</FinalAssembly>
</RCComponents>
</RecurringCosts>
<OperatingCosts>
<OperatingScenario Desc="Umrechnungsfaktor fuer verschiedene DOC-Einheiten, zusaetzlich aus A/C-XML: Nseats=PassengersTotal">
<FlightsPerYear Desc="Flights per year / take-offs annually; aus operating_company.xml" ToolLevel="1" Unit="">0</FlightsPerYear>
<SeatLoadFactor Desc="utilisation factor for the payload; aus operating_company.xml" ToolLevel="1" Unit="">0</SeatLoadFactor>
</OperatingScenario>
<DirectOperatingCosts>
<DOC_total Desc="Summe aller DOCComponents (s.u)">
<DOC_year Desc="DOC pro Jahr" ToolLevel="1" Unit="$/year">0</DOC_year>
<DOC_FH Desc="DOC pro Flugstunde = DOC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">0</DOC_FH>
<DOC_flight Desc="DOC pro Flug = DOC_year/(Nta)" ToolLevel="1" Unit="$/flight">0</DOC_flight>
<DOC_km Desc="DOC pro km = DOC_year/(Nta*R)" ToolLevel="1" Unit="$/km">0</DOC_km>
<DOC_100ASK Desc="DOC pro 100 Available Seat Kilometer = DOC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">0</DOC_100ASK>
</DOC_total>
<COC_total Desc="Summe aller DOCComponents ausser Depreciation und Insurance">
<COC_year Desc="COC pro Jahr" ToolLevel="1" Unit="$/year">0</COC_year>
<COC_FH Desc="COC pro Flugstunde = COC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">0</COC_FH>
<COC_flight Desc="COC pro Flug = COC_year/(Nta)" ToolLevel="1" Unit="$/flight">0</COC_flight>
<COC_km Desc="COC pro km = COC_year/(Nta*R)" ToolLevel="1" Unit="$/km">0</COC_km>
<COC_100ASK Desc="COC pro 100 Available Seat Kilometer = COC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">0</COC_100ASK>
</COC_total>
<DOCComponents Desc="DOC-Anteile in 100ASK">
<Charge Desc="Gebuehren pro 100ASK">
<ChargeTotal Desc="total charges" ToolLevel="1" Unit="$/100ASK">0</ChargeTotal>
<ChargesComponents>
<NavigationCharge Desc="navigational charges" ToolLevel="1" Unit="$/100ASK">0</NavigationCharge>
<LandingCharge Desc="landing charges" ToolLevel="1" Unit="$/100ASK">0</LandingCharge>
<LandingChargeComponents>
<NoiseCharge Desc="noise charges" ToolLevel="1" Unit="$/100ASK">0</NoiseCharge>
<NOxCharge Desc="NOx charges" ToolLevel="1" Unit="$/100ASK">0</NOxCharge>
<ChargeWithoutEmission Desc="landing charges without emissions (noise + NOx)" ToolLevel="1" Unit="$/100ASK">0</ChargeWithoutEmission>
</LandingChargeComponents>
<GroundCharge Desc="ground charges" ToolLevel="1" Unit="$/100ASK">0</GroundCharge>
</ChargesComponents>
</Charge>
<Depreciation Desc="Abschreibungskosten" ToolLevel="1" Unit="$/100ASK">0</Depreciation>
<Insurance Desc="Versicherungskosten" ToolLevel="1" Unit="$/100ASK">0</Insurance>
<Maintenance Desc="Wartungskosten">
<MaintenanceTotal Desc="Wartungskosten gesamt" ToolLevel="1" Unit="$/100ASK">0</MaintenanceTotal>
<MaintenanceComponents>
<Airframe Desc="Wartungskosten Airframe">
<AirframeTotal Desc="Wartungskosten Airframe gesamt" ToolLevel="1" Unit="$/100ASK">0</AirframeTotal>
<CostComponents>
<LabourCosts Desc="Arbeitskosten Wartung Airframe" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Materialkosten Wartung Airframe" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
<AirframeComponents Desc="Kostenwert fuer das ATA Kapitel">
<ATA21 Desc="Environmental Control System">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA21>
<ATA22 Desc="Autoflight">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA22>
<ATA23 Desc="Communications">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA23>
<ATA24 Desc="Electrical System">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA24>
<ATA25 Desc="Furnishing">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA25>
<ATA26 Desc="Fire Protection">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA26>
<ATA27 Desc="Flight Control System">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA27>
<ATA28 Desc="Fuel System">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA28>
<ATA29 Desc="Hydraulic System">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA29>
<ATA30 Desc="Ice and Rain Protection">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA30>
<ATA31 Desc="Instrumentation">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA31>
<ATA32 Desc="Landing Gear">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA32>
<ATA33 Desc="Lights">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA33>
<ATA34 Desc="Navigation">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA34>
<ATA35 Desc="Oxygen">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA35>
<ATA36 Desc="Pneumatic">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA36>
<ATA38 Desc="Water and Waste">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA38>
<ATA49 Desc="APU">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA49>
<ATA51 Desc="Structure">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA51>
<ATA52 Desc="Doors">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA52>
<ATA53 Desc="Fuselage">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA53>
<ATA54 Desc="Nacelles">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA54>
<ATA55 Desc="Stabilizers">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA55>
<ATA56 Desc="Windows">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA56>
<ATA57 Desc="Wings">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA57>
<ATA99 Desc="Routinearbeiten, hauptsaechlich Inspektion">
<TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
<CostComponents>
<LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
<MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
</CostComponents>
</ATA99>
</AirframeComponents>
</Airframe>
<Engine Desc="Wartungskosten Triebwerk" ToolLevel="1" Unit="$/100ASK">0</Engine>
</MaintenanceComponents>
</Maintenance>
<Fuel Desc="Spritkosten" ToolLevel="1" Unit="$/100ASK">0</Fuel>
<Crew Desc="Crew Kosten">
<CrewTotal Desc="Crew Kosten gesamt" ToolLevel="1" Unit="$/100ASK">0</CrewTotal>
<CrewComponents>
<FlightCrew Desc="Flight Crew Kosten" ToolLevel="1" Unit="$/100ASK">0</FlightCrew>
<CabinCrew Desc="Cabin Crew Kosten" ToolLevel="1" Unit="$/100ASK">0</CabinCrew>
</CrewComponents>
</Crew>
<Delay Desc="Verspaetungskosten" ToolLevel="1" Unit="$/100ASK">0</Delay>
</DOCComponents>
</DirectOperatingCosts>
<IndirectOperatingCosts>
<IOC_total Desc="Summe aller IOCComponents (s.u)">
<IOC_year Desc="IOC pro Jahr" ToolLevel="1" Unit="$/year">0</IOC_year>
<IOC_FH Desc="IOC pro Flugstunde = IOC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">0</IOC_FH>
<IOC_flight Desc="IOC pro Flug = IOC_year/(Nta)" ToolLevel="1" Unit="$/flight">0</IOC_flight>
<IOC_km Desc="IOC pro km = IOC_year/(Nta*R)" ToolLevel="1" Unit="$/km">0</IOC_km>
<IOC_100ASK Desc="IOC pro 100 Available Seat Kilometer = IOC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">0</IOC_100ASK>
</IOC_total>
</IndirectOperatingCosts>
</OperatingCosts>
<EndOfLifeCosts>
<EOLCTotal Desc="End-of-Life Costs" ToolLevel="1" Unit="$">0</EOLCTotal>
<EOLCTotalComponents>
<TransportToEoLSite Desc="Kosten fuer Transport zur Abwrack-Location" ToolLevel="1" Unit="$">0</TransportToEoLSite>
<DisassemblyAndDismantling Desc="Kosten fuer Dissassembly and Dismantling" ToolLevel="1" Unit="$">0</DisassemblyAndDismantling>
<Recycling Desc="Materialrecycling, bei negativem Wert Benefit durch Materialverkauf" ToolLevel="1" Unit="$">0</Recycling>
<Incineration Desc="Kosten fuer Verbrennung (inkl. shredding, mixing, incineration, and landfill of ash) " ToolLevel="1" Unit="$">0</Incineration>
<Landfill Desc="Kosten fuer Landfill" ToolLevel="1" Unit="$">0</Landfill>
</EOLCTotalComponents>
</EndOfLifeCosts>
</LCC>
</MonetaryValues>
<EcologicalValues Desc="Oekologische Bewertung">
<Noise Desc="Akustische Kenngroessen und Laermbewertungsmasse">
<NoisePathFiles>
<Departure Desc="Dateiname des Departure Path" ToolLevel="1">0</Departure>
<Approach Desc="Dateiname des Approach Path" ToolLevel="1">0</Approach>
</NoisePathFiles>
<NoiseCertificationLevels>
<LateralPoint>
<LateralFullPower Desc="EPNL Sideline Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</LateralFullPower>
<SPL Desc="dBA at lateral point" ToolLevel="1" Unit="dBA">0</SPL>
<Loudness Desc="Loudness at lateral point" ToolLevel="1" Unit="Sone">0</Loudness>
<Tonality Desc="Tonality at lateral point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
<Sharpness Desc="Sharpness at lateral point" ToolLevel="1" Unit="Acum">0</Sharpness>
<PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at lateral point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
</LateralPoint>
<FlyoverPoint>
<Flyover Desc="EPNL Flyover Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</Flyover>
<SPL Desc="dBA at flyover point" ToolLevel="1" Unit="dBA">0</SPL>
<Loudness Desc="Loudness at flyover point" ToolLevel="1" Unit="Sone">0</Loudness>
<Tonality Desc="Tonality at flyover point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
<Sharpness Desc="Sharpness at flyover point" ToolLevel="1" Unit="Acum">0</Sharpness>
<PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at flyover point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
</FlyoverPoint>
<ApproachPoint>
<Approach Desc="EPNL Approach Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</Approach>
<SPL Desc="dBA at approach point" ToolLevel="1" Unit="dBA">0</SPL>
<Loudness Desc="Loudness at approach point" ToolLevel="1" Unit="Sone">0</Loudness>
<Tonality Desc="Tonality at approach point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
<Sharpness Desc="Sharpness at approach point" ToolLevel="1" Unit="Acum">0</Sharpness>
<PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at approach point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
</ApproachPoint>
<CumulativeValues>
<EPNdB Desc="EPNL Cumulative Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</EPNdB>
<SPL Desc="Cumulative dBA at the three points" ToolLevel="1" Unit="dBA">0</SPL>
<Loudness Desc="Cumulative Loudness at the three points" ToolLevel="1" Unit="Sone">0</Loudness>
<Tonality Desc="Tonality at the three points" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
<Sharpness Desc="Sharpness at the three points" ToolLevel="1" Unit="Acum">0</Sharpness>
<PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at the three points" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
</CumulativeValues>
</NoiseCertificationLevels>
<CommunityNoiseLevels>
<TakeOff>
<SPL Desc="Sound Pressure Level 10km from brake release" ToolLevel="1" Unit="dBA">0</SPL>
<SPLarea>
<dBAthreshold1 Desc="Area of SPL higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold1>
<dBAthreshold2 Desc="Area of SPL higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold2>
</SPLarea>
<PNLarea>
<PNLthreshold1 Desc="Area of PNL higher or equal than 65 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold1>
<PNLthreshold2 Desc="Area of PNL higher or equal than 85 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold2>
</PNLarea>
<PNLTarea>
<PNLTthreshold1 Desc="Area of PNLT higher or equal than 65 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold1>
<PNLTthreshold2 Desc="Area of PNLT higher or equal than 85 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold2>
</PNLTarea>
<EPNLarea>
<EPNLthreshold1 Desc="Area of EPNL higher or equal than 65 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold1>
<EPNLthreshold2 Desc="Area of EPNL higher or equal than 85 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold2>
</EPNLarea>
<LoudnessArea>
<LoudnessThreshold1 Desc="Area of Zwickers loudness higher or equal than 65 Phon" ToolLevel="1" Unit="km2">0</LoudnessThreshold1>
<LoudnessThreshold2 Desc="Area of Zwickers loudness higher or equal than 85 Phon" ToolLevel="1" Unit="km2">0</LoudnessThreshold2>
</LoudnessArea>
<TonalityArea>
<TonalityThreshold1 Desc="Area of tonality higher or equal than 0.075 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold1>
<TonalityThreshold2 Desc="Area of tonality higher or equal than 0.15 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold2>
<TonalityThreshold3 Desc="Area of tonality higher or equal than 0.25 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold3>
<TonalityThreshold4 Desc="Area of tonality higher or equal than 0.35 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold4>
</TonalityArea>
<SharpnessArea>
<SharpnessThreshold1 Desc="Area of sharpness higher or equal than 0.75 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold1>
<SharpnessThreshold2 Desc="Area of sharpness higher or equal than 1.0 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold2>
</SharpnessArea>
<PsychoacousticAnnoyanceArea>
<PAthreshold1 Desc="Area of PA higher or equal than 10" ToolLevel="1" Unit="km2">0</PAthreshold1>
<PAthreshold2 Desc="Area of PA higher or equal than 20" ToolLevel="1" Unit="km2">0</PAthreshold2>
</PsychoacousticAnnoyanceArea>
<SELarea Desc="Sound Exposure Level area">
<dBA85 Desc="Area of Sound Exposure Level higher or equal than 85 dBA" ToolLevel="1" Unit="km2">0</dBA85>
<dBA75 Desc="Area of Sound Exposure Level higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBA75>
<dBA65 Desc="Area of Sound Exposure Level higher or equal than 65 dBA" ToolLevel="1" Unit="km2">0</dBA65>
<dBA55 Desc="Area of Sound Exposure Level higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBA55>
</SELarea>
</TakeOff>
<Approach>
<SPL Desc="Sound Pressure Level 15km from touchdown" ToolLevel="1" Unit="dBA">0</SPL>
<SPLarea>
<dBAthreshold1 Desc="Area of SPL higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold1>
<dBAthreshold2 Desc="Area of SPL higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold2>
</SPLarea>
<PNLarea>
<PNLthreshold1 Desc="Area of PNL higher or equal than 65 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold1>
<PNLthreshold2 Desc="Area of PNL higher or equal than 85 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold2>
</PNLarea>
<PNLTarea>
<PNLTthreshold1 Desc="Area of PNLT higher or equal than 65 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold1>
<PNLTthreshold2 Desc="Area of PNLT higher or equal than 85 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold2>
</PNLTarea>
<EPNLarea>
<EPNLthreshold1 Desc="Area of EPNL higher or equal than 65 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold1>
<EPNLthreshold2 Desc="Area of EPNL higher or equal than 85 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold2>
</EPNLarea>
<LoudnessArea>
<LoudnessThreshold1 Desc="Area of Zwickers loudness higher or equal than 65 Sone" ToolLevel="1" Unit="km2">0</LoudnessThreshold1>
<LoudnessThreshold2 Desc="Area of Zwickers loudness higher or equal than 85 Sone" ToolLevel="1" Unit="km2">0</LoudnessThreshold2>
</LoudnessArea>
<TonalityArea>
<TonalityThreshold1 Desc="Area of tonality higher or equal than 0.075 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold1>
<TonalityThreshold2 Desc="Area of tonality higher or equal than 0.10 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold2>
<TonalityThreshold3 Desc="Area of tonality higher or equal than 0.20 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold3>
<TonalityThreshold4 Desc="Area of tonality higher or equal than 0.25 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold4>
</TonalityArea>
<SharpnessArea>
<SharpnessThreshold1 Desc="Area of sharpness higher or equal than 0.75 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold1>
<SharpnessThreshold2 Desc="Area of sharpness higher or equal than 1.0 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold2>
</SharpnessArea>
<PsychoacousticAnnoyanceArea>
<PAthreshold1 Desc="Area of PA higher or equal than 10" ToolLevel="1" Unit="km2">0</PAthreshold1>
<PAthreshold2 Desc="Area of PA higher or equal than 20" ToolLevel="1" Unit="km2">0</PAthreshold2>
</PsychoacousticAnnoyanceArea>
<SELarea Desc="Sound Exposure Level area">
<dBA85 Desc="Area of Sound Exposure Level higher or equal than 85 dBA" ToolLevel="1" Unit="km2">0</dBA85>
<dBA75 Desc="Area of Sound Exposure Level higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBA75>
<dBA65 Desc="Area of Sound Exposure Level higher or equal than 65 dBA" ToolLevel="1" Unit="km2">0</dBA65>
<dBA55 Desc="Area of Sound Exposure Level higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBA55>
</SELarea>
</Approach>
<CumulativeValues>
<EPNdB Desc="85 EPNdB area sum for takeoff and approach" ToolLevel="1" Unit="EPNdB">0</EPNdB>
<SPL Desc="75 dBA area sum for takeoff and approach" ToolLevel="1" Unit="dBA">0</SPL>
<Loudness Desc="85 Phon loudness area sum for takeoff and approach" ToolLevel="1" Unit="Sone">0</Loudness>
<Tonality Desc="Tonality area sum for takeoff and approach - 0.1 t.u. for short-range and 0.2 t.u. for long-range AC" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
<Sharpness Desc="1.0 Acum sharpness area sum for takeoff and approach" ToolLevel="1" Unit="Acum">0</Sharpness>
<PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance of 10 area sum for takeoff and approach" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
</CumulativeValues>
</CommunityNoiseLevels>
</Noise>
<Emissions>
<Development Desc="Analyse der Entwicklungsphase fuer gesamtes Flugzeugprogramm">
<CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">0</CO2>
<H2O Desc="Wasser" ToolLevel="1" Unit="kg">0</H2O>
<NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">0</NOx>
<CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">0</CO>
<SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">0</SO2>
<CH4 Desc="Methan" ToolLevel="1" Unit="kg">0</CH4>
<PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0</PM10>
<N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
<PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
<NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
<HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">0</HC>
</Development>
<Production>
<CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">0</CO2>
<H2O Desc="Wasser" ToolLevel="1" Unit="kg">0</H2O>
<NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">0</NOx>
<CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">0</CO>
<SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">0</SO2>
<CH4 Desc="Methan" ToolLevel="1" Unit="kg">0</CH4>
<PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0</PM10>
<N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
<PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
<NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
<HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">0</HC>
</Production>
<Operations>
<CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">0</CO2>
<H2O Desc="Wasser" ToolLevel="1" Unit="kg">0</H2O>
<NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">0</NOx>
<CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">0</CO>
<SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">0</SO2>
<CH4 Desc="Methan" ToolLevel="1" Unit="kg">0</CH4>
<PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0</PM10>
<N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
<PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
<NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
<HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">0</HC>
<OperationComponents>
<ICAO_LTO Desc="Triebwerksemissionen bestimmt nach dem LTO-Cycle gemaess ICAO Engine Emission Database und Standardzeiten fuer eine (!) StudyMission">
<CO2 Desc="CO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</CO2>
<H2O Desc="H2O emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</H2O>
<SO2 Desc="SO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</SO2>
<HC Desc="HC emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</HC>
<CO Desc="CO emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</CO>
<NOx Desc="NOx emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</NOx>
<PM10 Desc="PM10 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</PM10>
</ICAO_LTO>
<Mission Desc="Environmental analysis of one study mission">
<LTOTimes Desc="Times of LTO phases (all phases under 3000 ft)">
<Total Desc="Taxi, Take-off, Climb Out and Approach time (LTO)" ToolLevel="1" Unit="min">0</Total>
<TaxiTime Desc="Time for taxi (ICAO: 26 min)" ToolLevel="1" Unit="min">0</TaxiTime>
<TakeOffTime Desc="Time for take-off (until 35ft) (ICAO: 0.7 min)" ToolLevel="1" Unit="min">0</TakeOffTime>
<ClimbOutTime Desc="Time for climb out (35 ft to 3000ft)(ICAO: 2.2 min)" ToolLevel="1" Unit="min">0</ClimbOutTime>
<ApproachTime Desc="Time for approach (from 3000 ft to stop)(ICAO: 4 min)" ToolLevel="1" Unit="min">0</ApproachTime>
</LTOTimes>
<LTO Desc="Triebwerksemissionen bestimmt nach dem LTO-Cycle mit Missionsanalyse fuer eine (!) StudyMission">
<CO2 Desc="CO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</CO2>
<H2O Desc="H2O emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</H2O>
<SO2 Desc="SO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</SO2>
<HC Desc="HC emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</HC>
<CO Desc="CO emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</CO>
<NOx Desc="NOx emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</NOx>
<PM10 Desc="PM10 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</PM10>
</LTO>
<Cruise Desc="Triebwerksemissionen des Reiseflugs fuer eine (!) StudyMission">
<CO2 Desc="CO2 emitted during cruise" ToolLevel="1" Unit="kg">0</CO2>
<H2O Desc="H2O emitted during cruise" ToolLevel="1" Unit="kg">0</H2O>
<SO2 Desc="SO2 emitted during cruise" ToolLevel="1" Unit="kg">0</SO2>
<HC Desc="HC emitted during cruise" ToolLevel="1" Unit="kg">0</HC>
<CO Desc="CO emitted during cruise" ToolLevel="1" Unit="kg">0</CO>
<NOx Desc="NOx emitted during cruise" ToolLevel="1" Unit="kg">0</NOx>
<PM10 Desc="PM10 emitted during cruise" ToolLevel="1" Unit="kg">0</PM10>
</Cruise>
</Mission>
</OperationComponents>
</Operations>
<EndOfLife>
<CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">0</CO2>
<H2O Desc="Wasser" ToolLevel="1" Unit="kg">0</H2O>
<NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">0</NOx>
<CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">0</CO>
<SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">0</SO2>
<CH4 Desc="Methan" ToolLevel="1" Unit="kg">0</CH4>
<PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0</PM10>
<N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
<PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
<NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
<HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">0</HC>
</EndOfLife>
</Emissions>
<CED Desc="Cumulative Energy Demand">
<CEDTotal Desc="End-of-Life Costs" ToolLevel="1" Unit="MJ">0</CEDTotal>
<CEDComponents>
<Development Desc="Development" ToolLevel="1" Unit="MJ">0</Development>
<Production Desc="Production" ToolLevel="1" Unit="MJ">0</Production>
<Operations Desc="Operation" ToolLevel="1" Unit="MJ">0</Operations>
<EndOfLife Desc="End of Life" ToolLevel="1" Unit="MJ">0</EndOfLife>
</CEDComponents>
</CED>
<ClimateImpact Desc="Climate Impact due to Aircraft Operation">
<ATR Desc="Average Temperatur Response per year for aircraft operating lifetime" ToolLevel="1" Unit="mK">0</ATR>
<AGTP Desc="Absolute Global Temperature Potential after final year of operation" ToolLevel="1" Unit="K">0</AGTP>
<AGTP100 Desc="Absolute Global Temperature Potential after 100 years" ToolLevel="1" Unit="K">0</AGTP100>
<AGWP Desc="Absolute Global Warming Potential after final year of operation" ToolLevel="1" Unit="(W/m2)*year">0</AGWP>
<AGWP100 Desc="Absolute Global Warming Potential after 100 years" ToolLevel="1" Unit="(W/m2)*year">0</AGWP100>
</ClimateImpact>
<AirQuality Desc="Climate Impact due to Aircraft Operation">
<ToleranceFactors Desc="Tolerance Factors of Emissions emitted during LTO" Unit="-">
<HC Desc="TF Kohlenwasserstoff" ToolLevel="1" Unit="-">0</HC>
<CO Desc="TF Kohlenmonoxid" ToolLevel="1" Unit="-">0</CO>
<NOx Desc="TF Stickoxide" ToolLevel="1" Unit="-">0</NOx>
<soot Desc="TF Russ" ToolLevel="1" Unit="-">0</soot>
</ToleranceFactors>
<AirQualityIndex Desc="Air Quality Index" ToolLevel="1" Unit="-">0</AirQualityIndex>
</AirQuality>
</EcologicalValues>
<Requirements Desc="Designforderungen">
<m_Payload Desc="Design-Nutzlast (z.B. Anzahl PAX*MassPerPAX, s. DesignSpecification/Accommodation/)" Unit="kg">17000</m_Payload>
<m_MaximumPayload Desc="Maximale Nutzlast i. a. (PAX + 2*Luggage, da Cargo ~ Luggage)" Unit="kg">20000</m_MaximumPayload>
<DesignMission Desc="Definition der Auslegungsmission mit Startstrecke, Steigleistung, Initial Cruise und Landestrecke">
<DeltaISA Default="0" Desc="Temperature deviation from ISA" Unit="K">0</DeltaISA>
<R_Design Desc="Auslegungsreichweite" Unit="NM">2500</R_Design>
<TOFL_Design Desc="Design takeoff distance (Balanced Field Length) at Sea Level with MTOM and (ISA + deltaISA)-Conditions" Unit="m">2122</TOFL_Design>
<TTC_Design Desc="Auslegungs- Time-to-Climb (von 1500 ft auf ICA bei ISA+deltaISA)" Unit="min">35</TTC_Design>
<ClimbGradients Desc="Steiggradientenforderungen">
<secondTOsegment Desc="Climb gradient in 2nd take-off segment" Unit="percent">2.4</secondTOsegment>
<finalTOsegment Desc="Climb gradient in final take-off segment" Unit="percent">1.2</finalTOsegment>
<approachAEO Desc="Approach gradient with all engine operating" Unit="percent">3.2</approachAEO>
<approachOEI Desc="Approach gradient with one engine inoperative" Unit="percent">2.1</approachOEI>
</ClimbGradients>
<ClimbSpeedSchedule Desc="Liste der Geschwindigkeiten im Steigflug CAS unter FL100; CAS ueber FL100; M_cruise ueber Crossover-Altitude. Ggf. nur die erste bzw. die ersten beiden Geschwindigkeiten (Prop).">
<ClimbSpeeds Desc="Anzahl der Climb-Speed der Schedule. 1 = eine CAS, 2 = CAS mit ATC-limit u. darueber, 3 = zwei CAS u. eine Machzahl">3</ClimbSpeeds>
<CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
<CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
<Delta_MclimbToMcruise Desc="Differenz der Machzahl ueber Crossover-Altitude zur Cruise Machzahl" Unit="-">-0.02</Delta_MclimbToMcruise>
</ClimbSpeedSchedule>
<DescentSpeedSchedule Desc="Liste der Geschwindigkeiten im Sinkflug CAS unter FL100; CAS ueber FL100; Standardmaessig M_cruise ueber Crossover-Altitude.">
<CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
<CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
</DescentSpeedSchedule>
<h_initialCruise_Design Desc="Erste Cruise-Altitude (TOC)" Unit="ft">33000</h_initialCruise_Design>
<M_initialCruise_Design Desc="Erste Cruise-Machzahl (TOC)" Unit="-">0.78</M_initialCruise_Design>
<LDN_Design Desc="Needed runway length at Sea Level with MLM and (ISA + deltaISA)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6)" Unit="m">2387</LDN_Design>
<V_ApproachSpeed_Design Desc="Auslegungsanfluggeschwindigkeit in KCAS, Approach Category A: 0-90 kts, B: 91-120 kts, C: 121-140 kts, D: 141-165 kts, E: greater 165 kts" Unit="KCAS">138</V_ApproachSpeed_Design>
<AlternateDistance Desc="Reichweite der Alternate Mission" Unit="NM">200</AlternateDistance>
<TakeOffProcedure Desc="Standard, ICAO-A, ICAO-B">Standard</TakeOffProcedure>
<ApproachProcedure Desc="Standard, CDA, CDA-Steep">Standard</ApproachProcedure>
<TaxiTimeOrigin Desc="Dauer des Taxiing beim Start" Unit="min">9</TaxiTimeOrigin>
<TaxiTimeDestination Desc="Dauer des Taxiing nach der Landung" Unit="min">5</TaxiTimeDestination>
</DesignMission>
<StudyMission Desc="Definition der Study-Mission mit Startstrecke, Steigleistung, Initial Cruise und Landestrecke">
<DeltaISA Default="0" Desc="Temperature deviation from ISA" Unit="K">0</DeltaISA>
<R_Design Desc="Auslegungsreichweite" Unit="NM">500</R_Design>
<m_Payload Desc="Nutzlast auf Study-Mission" Unit="kg">13608</m_Payload>
<NumberOfPAX Desc="Anzahl Passagiere auf Study-Mission" Unit="-">150</NumberOfPAX>
<ClimbSpeedSchedule Desc="Liste der Geschwindigkeiten im Steigflug CAS unter FL100; CAS ueber FL100; M_cruise ueber Crossover-Altitude. Ggf. nur die erste bzw. die ersten beiden Geschwindigkeiten (Prop).">
<ClimbSpeeds Desc="Anzahl der Climb-Speed der Schedule. 1 = eine CAS, 2 = CAS mit ATC-limit u. darueber, 3 = zwei CAS u. eine Machzahl">3</ClimbSpeeds>
<CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
<CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
<Delta_MclimbToMcruise Desc="Differenz der Machzahl ueber Crossover-Altitude zur Cruise Machzahl" Unit="-">-0.02</Delta_MclimbToMcruise>
</ClimbSpeedSchedule>
<DescentSpeedSchedule Desc="Liste der Geschwindigkeiten im Sinkflug CAS unter FL100; CAS ueber FL100; Standardmaessig M_cruise ueber Crossover-Altitude.">
<CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
<CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
</DescentSpeedSchedule>
<h_initialCruise Desc="Erste Cruise-Altitude (TOC)" Unit="ft">35000</h_initialCruise>
<M_initialCruise Desc="Erste Cruise-Machzahl (TOC)" Unit="-">0.78</M_initialCruise>
<AlternateDistance Desc="Reichweite der Alternate Mission" Unit="NM">200</AlternateDistance>
<TakeOffProcedure Desc="Standard, ICAO-A, ICAO-B">Standard</TakeOffProcedure>
<ApproachProcedure Desc="Standard, CDA, CDA-Steep">Standard</ApproachProcedure>
<TaxiTimeOrigin Desc="Dauer des Taxiing beim Start" Unit="min">9</TaxiTimeOrigin>
<TaxiTimeDestination Desc="Dauer des Taxiing nach der Landung" Unit="min">5</TaxiTimeDestination>
</StudyMission>
<FuelPlanningMethod Desc="Methode zur Tankschaetzung: JAR, FAR-Domestic, FAR-Flag (International)">JAR</FuelPlanningMethod>
<V_MaximumGroundspeed Desc="Maximale Rollgeschwindigkeit, durch das Tyre Speed Rating begrenzt in KCAS" Unit="KCAS">195</V_MaximumGroundspeed>
<DesignFlightEnvelope>
<VMO Desc="Max operating speed. IAS also die Strukturbestimmenden Staudruckgeschwindigkeit" Unit="KCAS">350</VMO>
<MMO Desc="Max operating Mach No." Unit="-">0.82</MMO>
<h_maxOperating Desc="Max operating Altitude" Unit="ft">38500</h_maxOperating>
<h_maxOEI Desc="Max operating Altitude One-Engine-Inoperative" Unit="ft">15000</h_maxOEI>
</DesignFlightEnvelope>
<SizeLimits Desc="maximale geometrische Abmasse">
<SpanLimit Desc="Spannweitenbegrenzung" Unit="m">36</SpanLimit>
</SizeLimits>
<ACN Desc="Aircraft Classification Number">
<ACNCatType Desc="ACN Pavement Type; flex oder rigid" Unit="-">flex</ACNCatType>
<ACNCategory Desc="ACN Pavement Strength; A, B, C oder D" Unit="-">B</ACNCategory>
<ACNLimit Desc="ACN Limit fuer die ausgewaehlte Kategorie" Unit="-">42</ACNLimit>
</ACN>
</Requirements>
<DesignSpecification Desc="Spezifikation des Entwurfs">
<Configuration Desc="Qualitative Beschreibung der Konfiguration">
<Wing Desc="Parameter des Fluegels">
<Position Desc="Fluegellage low, mid, high" Unit="-">low</Position>
</Wing>
<Stabiliser Desc="Parameter des Hoehenleitwerks">
<h_OverWing Desc="Vertikale Position bzgl. des Seitenleitwerks (0: conventional 1: T-Tail)" Unit="-">0</h_OverWing>
</Stabiliser>
<LandingGear Desc="Fahrwerksanordnung">
<MainGearPosition Desc="Position des Hauptfahrwerks (Wing oder Fuselage)">Wing</MainGearPosition>
<Retractable Desc="Switch for (non-)retractable LandingGear">1</Retractable>
<FrictionCoefficient Default="0.03" Desc="Friction coefficient of tyres and pavement: Raymer p.486 - Table 17.1: 0.03 - 0.05">0.03</FrictionCoefficient>
<BrakingCoefficient Default="0.34189" Desc="Raymer p.486 - Table 17.1: 0.3 - 0.5; Torenbeek: jet 0.4-0.5; prop 0.35-0.45; Airbus: Medium Deceleration = 11 ft/s^2 = 0.34189">0.34189</BrakingCoefficient>
</LandingGear>
<Fuselage Desc="Fuselage parameters">
<Pressurized Desc="Is the fuselage pressurized? 1 for yes, 0 for no">1</Pressurized>
</Fuselage>
<CertificationType Desc="Zertifizierung nach CS-23 oder CS-25">CS-25</CertificationType>
<Fin Desc="Parameter des Seitenleitwerks">
<FinConfig Desc="0: Conventional 1: H-Tail" Unit="-">0</FinConfig>
</Fin>
<SkinThickness Default="0" Desc="Skin thickness of profiles" Unit="m">0</SkinThickness>
</Configuration>
<Accommodation Desc="Vorgaben bezueglich der Passagierdecks und Klassen">
<MassPerPAX Desc="Masse pro PAX (z.B. PAX 75 kg + Luggage: Std.-Wert 90.72 kg (Quelle Airbus: All about the A320 family, Tech App.))" Unit="kg">90.72</MassPerPAX>
<PAXDecks Desc="Anzahl der Passagierdecks">1</PAXDecks>
<PAXDeck Desc="Passagierdeck mit Klassen in der Folge der Klassen-ID" ID="1">
<Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck">2</Classes>
<Class Desc="Definition der Klasse" ID="1">
<ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">business</ClassType>
<Seating Desc="Bestuhlung des Querschnitts">22</Seating>
<Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">12</Seats>
</Class>
<Class Desc="Definition der Klasse" ID="2">
<ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">economy</ClassType>
<Seating Desc="Bestuhlung des Querschnitts">33</Seating>
<Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">138</Seats>
</Class>
<Class Desc="Definition der Klasse" ID="3">
<ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">first</ClassType>
<Seating Desc="Bestuhlung des Querschnitts">22</Seating>
<Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">0</Seats>
</Class>
</PAXDeck>
</Accommodation>
<Cargo Desc="Vorgaben bezueglich der Frachtdecks und ULDs">
<CargoDecks Desc="Anzahl der Frachtdecks">1</CargoDecks>
<CargoDeck Desc="Cargodeck mit verschiedenen Containertypen" ID="1">
<Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck">2</Compartments>
<Compartment Desc="Definition des Compartments" ID="1">
<CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">forward</CompartmentType>
<ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes>
<ULDType Desc="Definition der Containergruppe" ID="1">
<ULD Desc="Normbezeichnung des ULD">LD3-45</ULD>
<ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow>
<ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">3</ULDs>
</ULDType>
</Compartment>
<Compartment Desc="Definition des Compartments" ID="2">
<CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">aft</CompartmentType>
<ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes>
<ULDType Desc="Definition der Containergruppe" ID="1">
<ULD Desc="Normbezeichnung des ULD">LD3-45</ULD>
<ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow>
<ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">4</ULDs>
</ULDType>
</Compartment>
<Compartment Desc="Definition des Compartments" ID="3">
<CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">bulk</CompartmentType>
<ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes>
<ULDType Desc="Definition der Containergruppe" ID="1">
<ULD Desc="Normbezeichnung des ULD">LD3-45</ULD>
<ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow>
<ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">1</ULDs>
</ULDType>
</Compartment>
</CargoDeck>
</Cargo>
<Propulsion Desc="Vorgaben zum Antriebssystem">
<TypeOfEngine Desc="Triebwerkstechnologie (Jet oder Prop)" Unit="-">Jet</TypeOfEngine>
<NumberOfEngines Desc="Anzahl der Triebwerke">2</NumberOfEngines>
<PositionOfEngines Desc="Positionierung der Triebwerke">
<EnginesOnWing Desc="Anzahl der Triebwerke am Fluegel">2</EnginesOnWing>
<EnginesOnFuselage Desc="Anzahl der Triebwerke am Rumpf, mit Pylons montiert">0</EnginesOnFuselage>
<EnginesInFuselage Desc="Anzahl der Triebwerke im Rumpf integriert">0</EnginesInFuselage>
<WingEnginePosition Desc="0=EngineUnderWing; 1= EnginesOverWing">0</WingEnginePosition>
</PositionOfEngines>
<NumberOfPropulsors Desc="Number of powertrains" ToolLevel="1">2</NumberOfPropulsors>
<Propulsor ID="1">
<TypeOfPropulsor Desc="Propulsion technology (Jet or Prop)" Unit="-">Jet</TypeOfPropulsor>
<PropulsorPosition>
<ParentComponentID Default="MainWing" Desc="ID of the component to which the propulsor is attached (MainWing, Fuselage)">MainWing</ParentComponentID>
<yPosition Desc="specific position (0=mid, 1=innerRight, -1=innerLeft, 2=outerRight, -2=outerLeft">1</yPosition>
<xPosition Desc="specific position (0=front, 1=back)">0</xPosition>
</PropulsorPosition>
</Propulsor>
<Propulsor ID="2">
<TypeOfPropulsor Desc="Propulsion technology (Jet or Prop)" Unit="-">Jet</TypeOfPropulsor>
<PropulsorPosition>
<ParentComponentID Default="MainWing" Desc="ID of the component to which the propulsor is attached (MainWing, Fuselage)">MainWing</ParentComponentID>
<yPosition Desc="specific position (0=mid, 1=innerRight, -1=innerLeft, 2=outerRight, -2=outerLeft">-1</yPosition>
<xPosition Desc="specific position (0=front, 1=back)">0</xPosition>
</PropulsorPosition>
</Propulsor>
<FuelDensity Desc="Density of fuel" Unit="kg/l">0.785</FuelDensity>
</Propulsion>
<TankConfiguration Desc="Vorgaben zur Aufteilung der Tanks">
<NumberOfCenterTanks Desc="Anzahl der Tanks im Rumpf (Fluegelkasten + zus. Tanks)">1</NumberOfCenterTanks>
<NumberOfWingTanks Desc="Anzahl der Tanks im Fluegel">2</NumberOfWingTanks>
<NumberOfTrimTanks Desc="Anzahl der Tanks zur Trimmung">0</NumberOfTrimTanks>
</TankConfiguration>
<HighLiftSystem Desc="Vorgaben zum Hochauftriebssystem">
<C_LmaxT-O Desc="Maximaler Auftriebsbeiwert in Startkonfiguration. Statistik, falls Wert 0" Unit="-">2.4</C_LmaxT-O>
<C_LmaxLanding Desc="Maximaler Auftriebsbeiwert in Landekonfiguration. Statistik, falls Wert 0" Unit="-">2.8</C_LmaxLanding>
</HighLiftSystem>
<DesignLoads Desc="Vorgaben zu zulaessigen Lastvielfachen">
<n1 Desc="maximum positive load limit (CS-25: n1=2.5g)" Unit="g">2.5</n1>
<n2 Desc="maximum negative load limit (CS-25: n2=-1.0g)" Unit="g">-1</n2>
<NormalManeuver Default="1.1" Desc="Normal used load factor for maneuvers (e.g. flare)">1.1</NormalManeuver>
</DesignLoads>
<Technology Desc="Vorgaben spezieller Technologien">
<LaminarFlow Desc="HLFC oder NLF">
<Components Desc="Flugzeugkomponenten, auf die HLFC/NLF angewendet wird">
<Wing>
<UpperSide Desc="Fluegeloberseite (HLFC, NLF, None)">None</UpperSide>
<LowerSide Desc="Fluegelunterseite (HLFC, NLF, None)">None</LowerSide>
</Wing>
<Stabilizer>
<UpperSide Desc="Fluegeloberseite (HLFC, NLF, None)">None</UpperSide>
<LowerSide Desc="Fluegelunterseite (HLFC, NLF, None)">None</LowerSide>
</Stabilizer>
<Fin Desc="Seitenleitwerk (HLFC, NLF, None)">None</Fin>
<Nacelles Desc="Triebwerksgondeln (HLFC, NLF, None)">None</Nacelles>
</Components>
<OperatingCondition>
<HLFConlyForCruise>1</HLFConlyForCruise>
<MinMachForHLFCActivation>0.78</MinMachForHLFCActivation>
</OperatingCondition>
</LaminarFlow>
<ElectricTaxiing>
<DoElectricTaxiing Desc="1: Electric Taxiing, 0: Propulsion Taxiing">0</DoElectricTaxiing>
<EngineWarmupTime Desc="Laufzeit der Triebwerke vor dem Start" Unit="min">0</EngineWarmupTime>
</ElectricTaxiing>
<BallisticRecoverySystem Desc="Ballistic Recovery System (Parachute)">0</BallisticRecoverySystem>
<VariableCamber Desc="Aircraft has VC segments">0</VariableCamber>
</Technology>
</DesignSpecification>
</AcftExchangeFile>