.jpg "RD3M-500 Turbojet engine © Konstantinos Panitsidis")
Photo from the personal collection of Konstantinos Panitsidis
Technical specifications 
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TECHNICAL SPECIFICATIONS
| Fuel | T-1, TS-1 |
| Oil | - |
| Max thrust take-off power rating | 9.646 kgf |
| Specific fuel consumption, take-off power rating | 1,0 kg/kgf.*h |
| Max thrust, cruise power | ~6.200 kgf |
| Specific fuel consumption, cruise power | 0,93 kg/kgf.*h |
| Pressure ratio, take-off power rating | 6,4 |
| Bypass ratio | - |
| Temperature of the gas at the turbine intake, take-off power rating | 1.130 K |
| Air flow rate, take-off power rating | 150 kg/sec |
| Compressor rotation frequency low-pressure, take-off power rating | - |
| Compressor rotation frequency high-pressure, take-off power rating | |
| Diameter | 1400 mm |
| Height | - |
| Width | - |
| Length | 5380 mm |
| Weight | 3.100 kg |
| Specified service life | - |
