RD-0103
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg LOx/Kerosene rocket engine. T-3, P-1 aircraft by Sukhoi. Out of Production. Based on RD-0102. Chamber pressure 37.3 - 15.7 bar.
Throttled thrust(vac): 13.700 kN (3,080 lbf). Chamber Pressure: 37.30 bar. Propellant Formulation: LOX/TS1.
Related
- Country
- Russia
- Propellants
- Lox/Kerosene
- Agency
- Kosberg bureau
- Bibliography
- 309