| Ishikawajima-Harima J3 ✕ | Westinghouse J34 ✕ | |
|---|---|---|
| Aircraft Engine Manufacturer | IHI Corporation | Westinghouse |
| Aircraft Engine Type | Turbojet | Turbojet |
| Dry Weight (kg) | 430 | 547.486 |
| Diameter (mm) | 627 | 685.8 |
| Length (mm) | 1661 | 2844.8 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Ishikawajima-Harima_J3 | en.wikipedia.org/wiki/Westinghouse_J34 |
| Fuel | JP-4 jet fuel | |
| Geared Fan | No | No |
| Combustion Chamber | annular combustion chamber with 30 fuel supply pipes and vapouriser tubes | Annular |
| Afterburner | No | No |
| Streams | 1 | 1 |
| Maximum Takeoff Thrust (kN) | 13.7 | 15.12 |
| Thrust To Weight | 3.2 | 2.82 |
| Specific Fuel Consumption (g/(kN·s)) | 3027.942 | |
| Compressor Description | eight-stage axial compressor | Single-spool, 11-stage axial |
| Turbine Description | single-stage axial-flow | 2-stage turbine |