Data for some military gas turbine engines
| Model No. | Type | Max thrust or power @ SLS | SFC at max |
Airflow (lb/sec) |
|
D (in) |
|
|
|
Remarks |
| J57-P-23 | TJ |
16,000 lb |
2.10 |
|
11.5 (16) |
40 | 246 | 5,169 | 1,600 | AB, F-102A, F-100D |
| J57-P-43WB | TJ |
11,200 lb |
0.775 |
|
12 (16) |
39 | 167.3 | 3,870 | 1,600 | Water-injected, KC-135 |
| J58-P | TJ |
*32,500 lb |
|
|
*6 (9) |
|
|
|
|
AB, YF-12A, SR-71 |
| J60-P-3 | TJ |
3,000 lb |
0.96 |
|
7 (9) |
23.4 | 79.5 | 460 | 1,600 | T-39A, C-140A |
| J69-T-25 | TJ |
1,025 lb |
1.14 |
|
3.9 (0,1) |
22.3 | 43.3 | 364 | 1,525 | T-37B |
| J75-P-17 | TJ |
24,500 lb |
2.15 |
|
12.0 (15) |
43 | 237.6 | 5,875 | 1,610 | AB, F-106A/B |
| J79-GE-17 | TJ |
17,820 lb |
1.965 |
|
13.5 (17) |
39.1 | 208.7 | 3,855 | 1,210 | AB, F-4E/G |
| J85-GE-5H | TJ |
3,850 lb |
2.20 |
|
7 (8) |
20.4 | 109.1 | 584 | 1,640 | AB, T-38A/B |
| J85-GE-17 | TJ |
2,850 lb |
0.99 |
|
7 (8) |
17.7 | 40.4 | 395 | 1,640 | A-37B |
| J85-GE-21 | TJ |
5,000 lb |
2.13 |
|
8 (8) |
20 | 116 | 667 | 1,790 | AB, F-5E/F |
| PT6A-42 | TP |
850 eshp |
0.601 |
|
8 (3,1) |
19 | 67 | 391 |
|
C-12E |
| PT6A-45R | TP |
1,197 eshp |
0.553 |
|
8.7 (3,1) |
19 | 72 | 434 |
|
C-23A |
| T400-CP-400 | TS |
1,800 shp |
0.606 |
|
7 (3, 1) |
43.5 | 66.3 | 716 | 1,920 | Bell UH-1N |
| T406-AD-400 | TS |
6,150 shp |
0.424 |
|
(14) |
24.5 | 77.9 | 975 | 1,422 | CV-22 |
| T53-L-13 | TS |
1,400 shp |
0.58 |
|
7 (5,1) |
23 | 47.6 | 549 | 1,720 | Bell UH-1H, AH-IG |
| T55-L-11 | TS |
3,750 shp |
0.52 |
|
8 (6,1) |
24.3 | 44 | 670 |
|
Boeing CH-47C |
| T56-A-7 | TP |
3,775 eshp |
0.528 |
|
9.45 (14) |
40.9 | 146 | 1,833 | 1,780 | C-130B/E/F |
| T56-A-15 | TP |
4,591 eshp |
0.54 |
|
9.55 (14) |
44.6 | 146.3 | 1,848 | 1,970 | C-130H/N/P |
| T58-GE-100 | TS |
1,500 shp |
0.606 |
|
8.4 (10) |
21.5 | 58.6 | 335 | 1,372 | Sikorsky CH-3E, HH-3E, F |
| T64-GE-100 | TS |
4,330 shp |
0.487 |
|
14 (14) |
20.2 | 77.1 | 720 | 1,520 | MH-53T |
| T700-GE-700 | TS |
1,622 shp |
0.46 |
|
15 (5,1) |
25 | 47 | 423 | 1,563 | UH-60A |
| T76-G-10 | TS |
715 shp |
0.60 |
|
8.6 (2) |
27.1 | 44.5 | 348 | 1,818 | OV-IOA |
TJ = turbojet, TP = turboprop, OPR = overall pressure ratio, TIT = turbine inlet temperature, TS = turboshaft,
(Stages) = (axial, centrifugal) compressor stages, SFC = specific fuel consumption.
*J-58 Reference: Lockheed SR-71 by Jay Miller, Aerofax Minigraph 1, Aerofax, Inc., Arlington, TX, 1985.
Sources: The Engine Handbook, Directorate of Propulsion, Headquarters Air Force Logistics Command, Wright-Patterson AFB, Ohio, 1991 and manufacturers’ literature.