AJ10-118F
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet Nitric acid/UDMH rocket engine. Used on Delta upper stage for Delta 0100, Delta 1000, N-2 boosters. First flight 1972.
Engine: 95 kg (209 lb). Chamber Pressure: 9.00 bar. Area Ratio: 40. Propellant Formulation: RFNA/UDMH. Thrust to Weight Ratio: 44.4. Coefficient of Thrust vacuum: 4.71652202294704. Coefficient of Thrust sea level: .27.
Related
- Family
- Storable liquid
- Country
- USA
- Launch Vehicles
- N-2, Delta 0100, Delta 1000
- Propellants
- Nitric acid/UDMH
- Stages
- Delta F
- Agency
- Aerojet