Data for some civil gas turbine engines
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Takeoff |
Cruise |
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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