|
The J75 was an advanced and larger version of the J57. The engine was in service from 1956 to 1967.
|
| Rated Output |
17,500 lbs thrust |
| Compressor |
Dual compressor, axial flow |
| Turbine |
1 stage axial |
| After Burner |
26,500 lbs thrust depending on series |
| Commonly Used On |
F-105, F-106A, F-107A, U-2A, P6M-, 707, DC-8 |
|
