AJ10-138
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet N2O4/Aerozine-50 rocket engine. Out of production. Originally developed for Vanguard and Able. Two used, thrust uprated from 3540 kgf to 3628 kgf, with higher specific impulse, in Transtage. Flown 1964-1980.
Engine: 110 kg (240 lb). Chamber Pressure: 7.00 bar. Area Ratio: 40. Thrust to Weight Ratio: 32.9863636363636. Oxidizer to Fuel Ratio: 2. Coefficient of Thrust vacuum: 4.39646147665109.
Related
- Family
- Storable liquid
- Country
- USA
- Launch Vehicles
- Titan IIIC, Titan IIIA, Titan 3C7
- Propellants
- N2O4/Aerozine-50
- Agency
- Aerojet