Report - Propulsion Design of SMR-2020
All outputs of the program 'propulsion_design' were created with version 3.0.0

Design Summary

Total Values

Parameter Value Unit
SLST246.822kN

Point Performance

Parameter Unit Max. T/O with offtakes Bucket Point with offtakes Bucket Point without offtakes
ThrustkN246.66241.936841.8736
Fuel Flowkg/s1.940670.6274190.589414
TSFC(kg/s)/N7.86771e-061.4961e-051.4076e-05

List of installed engines:

  • PW1127G-JM

Engine ID: 0

Parameter Value Unit
ModelPW1127G-JM-
Scale Factor1.02475-
SLST123.411kN
Mass3023.99kg
Bucket Thrust20.3592kN
Bucket TSFC1.5056e-05(kg/s)/N

Engine ID: 1

Parameter Value Unit
ModelPW1127G-JM-
Scale Factor1.02475-
SLST123.411kN
Mass3023.99kg
Bucket Thrust20.3592kN
Bucket TSFC1.5056e-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