Report - Propulsion Design of SMR-180-TF
All outputs of the program 'propulsion_design' were created with version 0.5.0

Design Summary

Total Values

Parameter Value Unit
SLST252.722kN

Point Performance

Parameter Unit Max. T/O with offtakes Bucket Point with offtakes Bucket Point without offtakes
ThrustkN252.72242.85642.9024
Fuel Flowkg/s1.985610.639750.603896
TSFC(kg/s)/N7.85688e-061.49279e-051.4076e-05

List of installed engines:

  • PW1127G-JM

Engine ID: 0

Parameter Value Unit
ModelPW1127G-JM-
Scale Factor1.04993-
SLST126.361kN
Mass3015.36kg
Bucket Thrust20.8489kN
Bucket TSFC1.50332e-05(kg/s)/N

Engine ID: 1

Parameter Value Unit
ModelPW1127G-JM-
Scale Factor1.04993-
SLST126.361kN
Mass3015.36kg
Bucket Thrust20.8489kN
Bucket TSFC1.50332e-05(kg/s)/N
Note: All bucket values are at the design flight condition with offtakes unless noted otherwise.

Bucket curve of the aircraft

Top view of the aircraft

Dimensions of nacelle_0

Dimensions of nacelle_1