R-40B
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Credit: Aerojet Redmond
Redmond N2O4/MMH rocket engine. In Production.
Engine: 7.23 kg (15.93 lb). Chamber Pressure: 10.34 bar. Area Ratio: 60. Restarts: 50000.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- N2O4/MMH
- Agency
- Redmond