RS-27C
USA
Original archive entry. The text, images and links below are kept as they were written.
Credit: Boeing / Rocketdyne
Rocke. First flight 1990.
Thrust (sl): 890.100 kN (200,102 lbf). Thrust (sl): 90,768 kgf. Engine: 1,091 kg (2,405 lb). Chamber Pressure: 48.00 bar. Area Ratio: 12. Thrust to Weight Ratio: 98.5320652356858. Oxidizer to Fuel Ratio: 2.245. Coefficient of Thrust vacuum: 1.47. Coefficient of Thrust sea level: 1.22.
Related
- Country
- USA
- Launch Vehicles
- Barbarian MDD, Delta 7925
- Propellants
- Lox/Kerosene
- Stages
- Delta Thor XLT-C
- Agency
- Rocketdyne