.jpg "R11F2-300 Turbojet engine © Konstantinos Panitsidis")
Photo from the personal collection of Konstantinos Panitsidis
Technical specifications 
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TECHNICAL SPECIFICATIONS
| Fuel | - |
| Oil | - |
| Max thrust take-off power rating | 3.977 kgf |
| Specific fuel consumption, take-off power rating | - |
| Max thrust, cruise power | - |
| Specific fuel consumption, cruise power | 0.94 kg/kgf. h |
| Pressure ratio, take-off power rating | 8,8 |
| Bypass ratio | - |
| Temperature of the gas at the turbine intake, take-off power rating | 1.175 K |
| Air flow rate, take-off power rating | - |
| Compressor rotation frequency low-pressure, take-off power rating | - |
| Compressor rotation frequency high-pressure, take-off power rating | |
| Diameter | 900 mm |
| Height | - |
| Width | - |
| Length | 4600 mm |
| Weight | 1088,5 kg |
| Specified service life | 1.500 h |
