AJ10-137
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet N2O4/Aerozine-50 rocket engine. Apollo SPS. Out of Production. Pressure-fed engine. Used as Apollo SM engine.
Chamber Pressure: 6.90 bar. Oxidizer to Fuel Ratio: 1.6.
Related
- Family
- Storable liquid
- Country
- USA
- Spacecraft
- Apollo CSM, Apollo CSM Block I, Apollo RM
- Propellants
- N2O4/Aerozine-50
- Agency
- Aerojet