RD-0120TD
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg tri-propellant (LOx/LH2/kerosene) rocket engine. Developed 1990's. 452s. Experimental version of the RD-0120 engine. Tested by supply of high-pressure kerosene from test bench or adapted existing kerosene pump for tests.
Throttled thrust(vac): 775.000 kN (174,226 lbf). Area Ratio: 85.7. Oxidizer to Fuel Ratio: 4.13.
Related
- Country
- Russia
- Propellants
- Lox/Kerosene/LH2, Lox/LH2
- Agency
- Kosberg bureau