diff --git a/CSMR/CSMR-2020/csmr-2020_startCSD.xml b/CSMR/CSMR-2020/csmr-2020_startCSD.xml
index 6931249be19fd7800b564d9343cc2844acfc1e46..fbfb182254433e77bb1e49bab31a022b10f0e229 100644
--- a/CSMR/CSMR-2020/csmr-2020_startCSD.xml
+++ b/CSMR/CSMR-2020/csmr-2020_startCSD.xml
@@ -8,7 +8,7 @@
<value>SMR-2020</value>
</model>
</general>
- <mission_files description="Name of xml files which are located in the missionData directory and contain the flight phase data" tool_level="0">
+ <mission_files description="Name of xml files which are located in the mission_data directory and contain the flight phase data" tool_level="0">
<design_mission_file description="Name of the design mission xml">
<value>design_mission.xml</value>
</design_mission_file>
@@ -21,58 +21,32 @@
</mission_files>
<design_specification description="Design specification">
<configuration description="Configuration information">
- <aerodynamic_technologies description="Integration of aerodynamic technologies on the aircraft: true / false">
- <value>false</value>
- </aerodynamic_technologies>
- <configuration_type description="aircraft configuration: tube_and_wing / blended_wing_body">
+ <configuration_type description="Aircraft configuration. Selector: tube_and_wing">
<value>tube_and_wing</value>
</configuration_type>
<fuselage_definition description="Design description of the fuselage.">
- <fuselage_type description="Fuselage type: single_aisle / wide_body">
+ <fuselage_type description="Fuselage type. Selector: single_aisle / wide_body">
<value>single_aisle</value>
</fuselage_type>
- <fuselage_pressurization description="Switch to select a pressurized fuselage. (true: pressurized fuselage, false: non pressurized fuselage)">
+ <fuselage_pressurization description="Switch to enable pressurized fuselage. Switch: true (On) / false (Off)">
<value>true</value>
</fuselage_pressurization>
- <blended_wing_body_configuration description="Additional design description for blended wing body configurations.">
- <number_of_payload_tubes description="Number of fuselage tubes for blendend wing body configurations. For tube and wing configuration is set to 1.">
- <value>1</value>
- <unit>1</unit>
- <default>1</default>
- <lower_boundary>1</lower_boundary>
- <upper_boundary>5</upper_boundary>
- </number_of_payload_tubes>
- <center_body_wing_sweep description="Sweep of the leading edge of the center body.">
- <value>60</value>
- <unit>degree</unit>
- <default>60</default>
- <lower_boundary>0</lower_boundary>
- <upper_boundary>75</upper_boundary>
- <center_body_wing_sweep_tolerance Desc="Permissible deviation of the actual from the desired leading edge sweep of the center body.">
- <value>5</value>
- <unit>degree</unit>
- <default>5</default>
- <lower_boundary>0</lower_boundary>
- <upper_boundary>15</upper_boundary>
- </center_body_wing_sweep_tolerance>
- </center_body_wing_sweep>
- </blended_wing_body_configuration>
</fuselage_definition>
<wing_definition description="Definitions for wing design">
- <mounting description="wing mounting for tube_and_wing configuration (ignored at blended_wing_body) - low / mid / high">
+ <mounting description="Wing mounting. Selector: low">
<value>low</value>
</mounting>
</wing_definition>
<empennage_definition description="Definitions for empennage design">
- <empennage_type description="tube_and_wing configuration: conventional - blended_wing_body: vertical_tails">
+ <empennage_type description="Empennage type. Selector: conventional">
<value>conventional</value>
</empennage_type>
</empennage_definition>
<undercarriage_definition description="Design description of the undercarriage.">
- <main_gear_mounting description="Mounting position of the main landing gear: wing_mounted / fuselage_mounted.">
+ <main_gear_mounting description="Mounting position of the main landing gear. Selector: wing_mounted / fuselage_mounted">
<value>wing_mounted</value>
</main_gear_mounting>
- <undercarriage_retractability description="Switch to set retractability of landing gear: retractable / non_retractable.">
+ <undercarriage_retractability description="Set retractability of landing gear. Selector: retractable / non_retractable">
<value>retractable</value>
</undercarriage_retractability>
</undercarriage_definition>
@@ -84,13 +58,13 @@
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
- <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
+ <location description="Component where the tank is located. Selector: fuselage / wing / horizontal_stabilizer">
<value>wing</value>
</location>
- <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total">
+ <position description="Position of tank in location. Selector: center / inner_left / outer_left / inner_right / outer_right / total">
<value>inner_left</value>
</position>
- <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+ <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Equals 0.0 for kerosene tanks. Only relevant for liquid hydrogen (not impemented yet). ">
<value>0.0</value>
<unit>1</unit>
<lower_boundary>0.0</lower_boundary>
@@ -107,10 +81,10 @@
<location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
<value>wing</value>
</location>
- <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total">
+ <position description="Position of tank in location. Selector: center / inner_left / outer_left / inner_right / outer_right / total">
<value>outer_left</value>
</position>
- <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+ <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Equals 0.0 for kerosene tanks. Only relevant for liquid hydrogen (not impemented yet). ">
<value>0.0</value>
<unit>1</unit>
<lower_boundary>0.0</lower_boundary>
@@ -127,10 +101,10 @@
<location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
<value>wing</value>
</location>
- <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total">
+ <position description="Position of tank in location. Selector: center / inner_left / outer_left / inner_right / outer_right / total">
<value>inner_right</value>
</position>
- <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+ <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Equals 0.0 for kerosene tanks. Only relevant for liquid hydrogen (not impemented yet). ">
<value>0.0</value>
<unit>1</unit>
<lower_boundary>0.0</lower_boundary>
@@ -147,10 +121,10 @@
<location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
<value>wing</value>
</location>
- <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total">
+ <position description="Position of tank in location. Selector: center / inner_left / outer_left / inner_right / outer_right / total">
<value>outer_right</value>
</position>
- <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+ <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Equals 0.0 for kerosene tanks. Only relevant for liquid hydrogen (not impemented yet). ">
<value>0.0</value>
<unit>1</unit>
<lower_boundary>0.0</lower_boundary>
@@ -167,50 +141,10 @@
<location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
<value>wing</value>
</location>
- <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total">
+ <position description="Position of tank in location. Selector: center / inner_left / outer_left / inner_right / outer_right / total">
<value>center</value>
</position>
- <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
- <value>0.0</value>
- <unit>1</unit>
- <lower_boundary>0.0</lower_boundary>
- <upper_boundary>1.0</upper_boundary>
- </energy_share>
- </tank>
- <tank ID="5" description="Additional center tank">
- <energy_carrier_ID description="see energy carrier specification node">
- <value>0</value>
- <unit>1</unit>
- <lower_boundary>0</lower_boundary>
- <upper_boundary>5</upper_boundary>
- </energy_carrier_ID>
- <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
- <value>fuselage</value>
- </location>
- <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total">
- <value>center</value>
- </position>
- <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
- <value>0.0</value>
- <unit>1</unit>
- <lower_boundary>0.0</lower_boundary>
- <upper_boundary>1.0</upper_boundary>
- </energy_share>
- </tank>
- <tank ID="6" description="Trim tank">
- <energy_carrier_ID description="see energy carrier specification node">
- <value>0</value>
- <unit>1</unit>
- <lower_boundary>0</lower_boundary>
- <upper_boundary>5</upper_boundary>
- </energy_carrier_ID>
- <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
- <value>horizontal_stabilizer</value>
- </location>
- <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total">
- <value>total</value>
- </position>
- <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+ <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Equals 0.0 for kerosene tanks. Only relevant for liquid hydrogen (not impemented yet). ">
<value>0.0</value>
<unit>1</unit>
<lower_boundary>0.0</lower_boundary>
@@ -219,20 +153,20 @@
</tank>
</tank_definition>
<loads description="Loads information">
- <design_load_factor description="design load factor n">
- <maximum description="maximum design load factor n">
+ <design_load_factor description="Design load factor n">
+ <maximum description="Maximum design load factor n">
<value>2.5</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>4</upper_boundary>
</maximum>
- <minimum description="maximum design load factor n">
+ <minimum description="Minimum design load factor n">
<value>-1.0</value>
<unit>1</unit>
<lower_boundary>-2.0</lower_boundary>
<upper_boundary>0.0</upper_boundary>
</minimum>
- <maneuver description="standard maneuver load factor for e.g. flare">
+ <maneuver description="Standard maneuver load factor for e.g. flare">
<value>1.1</value>
<unit>1</unit>
<lower_boundary>0.0</lower_boundary>
@@ -240,6 +174,9 @@
</maneuver>
</design_load_factor>
</loads>
+ <aerodynamic_technologies description="Integration of aerodynamic technologies on the aircraft: Switch: false (no additional aerodynamic technologies are considered)">
+ <value>false</value>
+ </aerodynamic_technologies>
</configuration>
<transport_task description="Define the transport task for aircraft project.">
<passenger_definition description="Define the masses of the passengers">
@@ -255,14 +192,14 @@
<lower_boundary>50</lower_boundary>
<upper_boundary>200</upper_boundary>
</mass_per_passenger>
- <luggage_mass_per_passenger description="Design mass of a the luggage for a single passenger">
+ <luggage_mass_per_passenger description="Design mass of the luggage for a single passenger">
<value>15</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>25</upper_boundary>
</luggage_mass_per_passenger>
</passenger_definition>
- <multi_passenger_deck_layout description="Switch to select a multi passenger deck fuselage design. (true: multi passenger deck allowed, false: multi passenger deck denied)">
+ <multi_passenger_deck_layout description="Switch to select a multi passenger deck fuselage design. Switch: true (On) / false (Off)">
<value>false</value>
<default>false</default>
<specific_number_of_passenger_decks>
@@ -295,7 +232,7 @@
</transport_task>
<energy_carriers description="Energy carriers information">
<energy_carrier ID="0" description="One specific energy carrier">
- <type description="Energy type (for multifuel engine create new ID). Selector: kerosene / liquid_hydrogen / battery / saf">
+ <type description="Energy type (for multifuel engine create new ID). Selector: kerosene">
<value>kerosene</value>
</type>
<density description="Energy carrier density.">
@@ -304,13 +241,13 @@
<lower_boundary>0</lower_boundary>
<upper_boundary>10000</upper_boundary>
</density>
- <volumetric_density description="Volumetric energy density of energy carrier.">
- <value>33.833.500.000</value>
+ <volumetric_density description="Volumetric energy density of energy carrier">
+ <value>3.38335e+10</value>
<unit>J/m^3</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1e+12</upper_boundary>
</volumetric_density>
- <gravimetric_density description="Gravimetric energy density of energy carrier.">
+ <gravimetric_density description="Gravimetric energy density of energy carrier">
<value>43100000</value>
<unit>J/kg</unit>
<lower_boundary>0</lower_boundary>
@@ -320,27 +257,27 @@
</energy_carriers>
<propulsion description="Propulsion information">
<propulsor ID="0" description="Information for specific propulsor">
- <powertrain description="Way the power is generated from the source. Selector: turbo / electric / fuel_cell">
+ <powertrain description="Way the power is generated from the source. Selector: turbo">
<value>turbo</value>
</powertrain>
- <type description="Type of main thrust generator. Selector: fan / prop">
+ <type description="Type of main thrust generator. Selector: fan">
<value>fan</value>
</type>
- <position description="propulsor position (arrangement order acc to ID order)">
- <parent_component description="position on component. Selector: wing / fuselage / empennage">
+ <position description="Propulsor position (arrangement order acc to ID order)">
+ <parent_component description="Position on component. Selector: wing / fuselage / empennage">
<value>wing</value>
</parent_component>
- <x description="x-position (aircraft coordinate system). Selector: front / back">
+ <x description="X-position (aircraft coordinate system). Selector: front / back">
<value>front</value>
</x>
- <y description="y position (aircraft coordinate system). Selector: left / right">
+ <y description="Y-position (aircraft coordinate system). Selector: left / right">
<value>left</value>
</y>
- <z description="z position (aircraft coordinate system). Selector: over / mid / under / in">
+ <z description="Z-position (aircraft coordinate system). Selector: over / mid / under / in">
<value>under</value>
</z>
</position>
- <energy_carrier_ID description="see energy carrier specification node">
+ <energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
@@ -354,27 +291,27 @@
</thrust_share>
</propulsor>
<propulsor ID="1" description="Information for specific propulsor">
- <powertrain description="Way the power is generated from the source. Selector: turbo / electric / fuel_cell">
+ <powertrain description="Way the power is generated from the source. Selector: turbo">
<value>turbo</value>
</powertrain>
- <type description="Type of main thrust generator. Selector: fan / prop">
+ <type description="Type of main thrust generator. Selector: fan">
<value>fan</value>
</type>
- <position description="propulsor position (arrangement order acc to ID order)">
- <parent_component description="position on component. Selector: wing / fuselage / empennage">
+ <position description="Propulsor position (arrangement order acc to ID order)">
+ <parent_component description="Position on component. Selector: wing / fuselage / empennage">
<value>wing</value>
</parent_component>
- <x description="x-position (aircraft coordinate system). Selector: front / back">
+ <x description="X-position (aircraft coordinate system). Selector: front / back">
<value>front</value>
</x>
- <y description="y position (aircraft coordinate system). Selector: left / right">
+ <y description="Y-position (aircraft coordinate system). Selector: left / right">
<value>right</value>
</y>
- <z description="z position (aircraft coordinate system). Selector: over / mid / under / in">
+ <z description="Z-position (aircraft coordinate system). Selector: over / mid / under / in">
<value>under</value>
</z>
</position>
- <energy_carrier_ID description="see energy carrier specification node">
+ <energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
@@ -387,9 +324,9 @@
<upper_boundary>1</upper_boundary>
</thrust_share>
</propulsor>
- <energy_provider description="source where energy is coming from per segment">
- <ground description="source where energy is coming from in the ground mission segment">
- <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <energy_provider description="Source where energy is coming from per segment">
+ <ground description="Source where energy is coming from in the ground mission segment">
+ <powertrain description="Way the power is generated from the source. Selector: propulsor / turbo / electric">
<value>turbo</value>
</powertrain>
<energy_carrier_ID description="see energy carrier specification node">
@@ -400,7 +337,7 @@
</energy_carrier_ID>
</ground>
<taxi description="source where energy is coming from in the taxi mission segment">
- <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <powertrain description="Way the power is generated from the source. Selector: propulsor / turbo / electric">
<value>turbo</value>
</powertrain>
<energy_carrier_ID description="see energy carrier specification node">
@@ -411,7 +348,7 @@
</energy_carrier_ID>
</taxi>
<takeoff description="source where energy is coming from in the takeoff mission segment">
- <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <powertrain description="Way the power is generated from the source. Selector: propulsor / turbo / electric">
<value>turbo</value>
</powertrain>
<energy_carrier_ID description="see energy carrier specification node">
@@ -422,7 +359,7 @@
</energy_carrier_ID>
</takeoff>
<climb description="source where energy is coming from in the climb mission segment">
- <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <powertrain description="Way the power is generated from the source. Selector: propulsor / turbo / electric">
<value>turbo</value>
</powertrain>
<energy_carrier_ID description="see energy carrier specification node">
@@ -433,7 +370,7 @@
</energy_carrier_ID>
</climb>
<cruise description="source where energy is coming from in the cruise mission segment">
- <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <powertrain description="Way the power is generated from the source. Selector: propulsor / turbo / electric">
<value>turbo</value>
</powertrain>
<energy_carrier_ID description="see energy carrier specification node">
@@ -444,7 +381,7 @@
</energy_carrier_ID>
</cruise>
<descent description="source where energy is coming from in the descent mission segment">
- <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <powertrain description="Way the power is generated from the source. Selector: propulsor / turbo / electric">
<value>turbo</value>
</powertrain>
<energy_carrier_ID description="see energy carrier specification node">
@@ -455,7 +392,7 @@
</energy_carrier_ID>
</descent>
<landing description="source where energy is coming from in the landing mission segment">
- <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <powertrain description="Way the power is generated from the source. Selector: propulsor / turbo / electric">
<value>turbo</value>
</powertrain>
<energy_carrier_ID description="see energy carrier specification node">
@@ -468,7 +405,7 @@
</energy_provider>
</propulsion>
<skinning description="Skinning Information">
- <material description="Material of skinning">
+ <material description="Material of skinning. Selector: aluminium2024">
<value>aluminium2024</value>
</material>
<thickness description="Thickness of skinning">
@@ -479,14 +416,14 @@
</thickness>
</skinning>
<technology>
- <variable_camber description="Switch if variable camber is used">
+ <variable_camber description="Switch if variable camber is used. Switch: false (Off)">
<value>false</value>
</variable_camber>
</technology>
</design_specification>
<requirements description="Aircraft design requirements">
<top_level_aircraft_requirements description="Top level aircraft requirements (TLAR)">
- <maximum_structrual_payload_mass description="Maximum structual payload mass which can be carried by the aircraft (e.g. for short trips)">
+ <maximum_structrual_payload_mass description="Maximum payload mass which can be carried by the aircraft (e.g. for short trips)">
<value>19300</value>
<unit>kg</unit>
<lower_boundary>100</lower_boundary>
@@ -498,7 +435,7 @@
<lower_boundary>600</lower_boundary>
<upper_boundary>5000</upper_boundary>
</takeoff_distance>
- <landing_field_length description="Needed runway length at Sea Level with maximum landiung mass (MLM) and (ISA + deltaISA)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6)">
+ <landing_field_length description="Needed runway length at Sea Level with maximum landing mass (MLM) and (ISA + deltaISA)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6)">
<value>2425.67</value>
<unit>m</unit>
<lower_boundary>600</lower_boundary>
@@ -545,7 +482,7 @@
<upper_boundary>1</upper_boundary>
</climb_or_descend_segment_gradient>
</flight_envelope>
- <pavement_classification_number description="Runway pavment classification number (PCN) - limits the maximum allowed aircraft classification number of undercarriage.">
+ <pavement_classification_number description="Runway pavement classification number (PCN) - limits the maximum allowed aircraft classification number of undercarriage">
<value>55</value>
<unit>1</unit>
<lower_boundary>5</lower_boundary>
@@ -558,37 +495,37 @@
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</delta_ISA>
- <range description="Target range for the specified mission">
+ <range description="Target range for design mission">
<value>4537400</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>20000000</upper_boundary>
</range>
- <contingency description="Reserved Fuel Percentage">
+ <contingency description="Contingency fuel in percentage (reserve fuel)">
<value>0.06</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>0.08</upper_boundary>
</contingency>
- <alt_dist description="Reserved fuel - alternate distance">
+ <alt_dist description="Alternate distance in m (reserve fuel)">
<value>370400</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>926000</upper_boundary>
</alt_dist>
- <loiter_time description="Reserved fuel - loiter time in seconds">
+ <loiter_time description="Loiter time in seconds (reserve fuel)">
<value>1800</value>
<unit>s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>3600</upper_boundary>
</loiter_time>
- <initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise.">
+ <initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise">
<value>0.78</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</initial_cruise_mach_number>
- <initial_cruise_altitude description="Initial cruise altitude (ICA) at top of descent. May be altered during cruise.">
+ <initial_cruise_altitude description="Initial cruise altitude (ICA) at top of descent. May be altered during cruise">
<value>10058.4</value>
<unit>m</unit>
<lower_boundary>1000</lower_boundary>
@@ -647,19 +584,19 @@
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</delta_ISA>
- <range description="Target range for the specified mission">
+ <range description="Target range for the study mission">
<value>1481600</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>20000000</upper_boundary>
</range>
- <initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise.">
+ <initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise">
<value>0.78</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</initial_cruise_mach_number>
- <initial_cruise_altitude description="Initial cruise altitude at top of descent. May be altered during cruise.">
+ <initial_cruise_altitude description="Initial cruise altitude at top of descent. May be altered during cruise">
<value>10668</value>
<unit>m</unit>
<lower_boundary>1000</lower_boundary>