RD-3A
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko LOx/Alcohol rocket engine. R-3A. Out of Production. Project for R-3A experimental missile. Stopped in favor of RD-103.
Thrust (sl): 390.000 kN (87,670 lbf). Engine: 885 kg (1,951 lb). Propellant Formulation: Lox/Alcohol-96%. Oxidizer to Fuel Ratio: 0.
Related
- Country
- Russia
- Launch Vehicles
- R-3A
- Propellants
- Lox/Alcohol
- Agency
- Glushko bureau