Data for some civil gas turbine engines

 

 


Takeoff


Cruise

 

Model no.

Manufacturer


Thrust (lb)


BR


OPR


Airflow (lb/sec)


Alt (kft)


Mach


Thrust (lb)


TSFC

Aircraft application

AE3007

Rolls-Royce


8,600


4.8


20






Embraer 37, Global Hawk UAV

CF6-50-C2

General Electric


52,500


4.31


30.4


1,476


35


0.80


11,555


0.630

DC1O-l0, A300B, 747-200

CF6-80-C2

General Electric


52,500


5.31


27.4


1,650


35


0.80


12,000


0.576

767-200, -300, -200ER

CF34-8

General Electric


14,500


5


28






0.68

Bombardier CRJ700, Embraer 170/175

GE90-B4

General Electric


87,400


8.40


39.3


3,037


35


0.80


17,500


777

GEnx

General Electric


53,000-75,000


10


42




0.85



787, 747-8

GP7270

Engine Alliance


70,000


8.7 *


45.6 +



35


0.85


12,633


A380

JT8D-15A

Pratt & Whitney


15,500


1.04


16.6


327


30


0.80


4.920


0.779

727, 737, DC9

JT9D-59A

Pratt & Whitney


53,000


4.90


24.5


1,639


35


0.85


11,950


0.646

DC1O-40, A300B, 747-200

PW2037

Pratt & Whitney


38,250


6.00


27.6


1,210


35


0.85


6,500


0.582

757-200

PW4052

Pratt & Whitney


52,000


5.00


27.5


1,700





767, A310-300

PW4084

Pratt & Whitney


87,900


6.41


34.4


2,550


35


0.83



777

CFM56-3C

CFM International


23,500


6.00


22.6


655


35


0.80


5,540


0.648

737-300, -400, -500

CFM56-5C

CFM International


31,200


6.60


31.5


1,027


35


0.80


6,600


0.545

A340

RB211-524B

Rolls Royce


50,000


4.50


28.4


1.513


35


0.85


11,000


0.643

Ll0ll-200, 747-200

RB211-535E

Rolls Royce


40,100


4.30


25.8


1.151


35


0.80


8,495


0.607

757-200

RB211-882

Rolls Royce


84,700


6.01


39.0


2,640


35


0.83


16,200


0.557

777

Trent 900

Rolls-Royce


70,000-76,000


8.7-8.5



2,655-2,745





A380

Trent 1000

Rolls-Royce


53,000-75,000


10-11



2400-2670





787

V2528-D5

International Aero Engines


28,000


4.70


30.5


825


35


0.80


5,773


0.574

MD-90

ALF502R-5

Honeywell


6,970


5.70


12.2



25


0.70


2,250


0.720

BAe 146-200, -200

TFE731-5

Honeywell


4,500


3.34


14.4


140


40


0.80


986


0.771

BAe 125-800

PW300

Pratt & Whitney Canada


4,750


4.50


23.0


180


40


0.80


1,113


0.675

BAe 1000

FJ44

Williams Rolls


1,900


3.28


12.8


63.3


30


0.70


600


0.750

 

Olympus 593

Rolls Royce/SNECMA


38,000


0


*11.3


410


53


2.00


10,030


1.190

Concorde

OPR = overall pressure ratio, TSFC = thrust specific fuel consumption, BR = bypass ratio

* at Cruise + Max Climb

Sources: The Engine Handbook, Directorate of Propulsion, Headquarters Air Force Logistics Command, Wright-Patterson AFB, Ohio, 1991 and manufacturers’ literature