RD-502
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
NPO Enerogmash Museum, November 1992
Credit: © Dietrich Haeseler
Glushko H2O2/Pentaborane rocket engine. Experimental upper stage engine. Developed 1960-66. Experimental upper stage engine. Program stopped due to toxicity of propellants. Intended for Proton upper stage. First flight 1966.
Initially proposed by Glushko for N-1 in September 1960.
Engine: 132 kg (291 lb). Chamber Pressure: 147.00 bar. Thrust to Weight Ratio: 75.75.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- H2O2/Pentaborane
- Agency
- Glushko bureau
- Bibliography
- 317