X-405
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
GE LOx/Kerosene rocket engine. Vanguard 1st stage. First flight 1957.
Thrust (sl): 123.800 kN (27,831 lbf). Thrust (sl): 12,625 kgf. Engine: 191 kg (421 lb). Chamber Pressure: 42.00 bar. Area Ratio: 5.5. Thrust to Weight Ratio: 71.9633507853403. Coefficient of Thrust vacuum: 1.81140659230715. Coefficient of Thrust sea level: 1.68045421135476.
Related
- Country
- USA
- Launch Vehicles
- Vanguard
- Propellants
- Lox/Kerosene
- Stages
- Vanguard-1
- Agency
- GE