MR-120
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Credit: Aerojet Redmond
Redmond Hydrazine rocket engine. Small ICBM. In Production. Developed as an attitude control thruster for the small ICBM.
Engine: 0.41 kg (0.90 lb). Chamber Pressure: 12.40 bar. Area Ratio: 15. Restarts: 1911.
Related
- Family
- Storable liquid
- Country
- USA
- Launch Vehicles
- SICBM
- Agency
- Redmond