Civil Engine Data

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
1,476
35
0.80
11,555
0.630 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

		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	1,476	35	0.80	11,555	0.630	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