J79
The J79 is a single-shaft turbojet engine with afterburner. It has been manufactured by MTU under license from General Electric since 1970. The engine's first application was the Lockheed F104G Starfighter, and a modified version has been powering the McDonnell Douglas F-4 Phantom II aircraft of the German armed forces since 1973.
Now that production has ended, MTU focuses on the repair and maintenance of the J79 engines.
| Technical Data | |
|---|---|
| Max. thrust afterburner | 79.6 kN |
| Max. thrust without afterburner | 52.8 kN |
| Air mass flow (take-off) | 77 kg/s |
| Pressure ratio (take-off) | 13.5:1 |
| Speed (100%) | 7460 rpm |
| Turbine entry temperature | 1261 K |
| Length | 5301 mm |
| Weight | 1724 kg |
Facts:
- Single-shaft turbojet engine with afterburner
- Seventeen-stage compressor
- Three-stage turbine
- Can-type combustion chamber
Support:
- Maintenance and repair of engines and modules under the "cooperative model" at MTU Aero Engines in Munich
- Technical-logistic support
Application & Partners
![]() |
||
| Phantom F4 |
MTU share: 32%
Partner:
- General Electric

Print
