LR105-3
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Rocketdyne LOx/Kerosene rocket engine. Out of Production. Early version of Atlas Sustainer. Gas generator, pump-fed.
Thrust (sl): 267.000 kN (60,023 lbf). Thrust (sl): 27,200 kgf. Chamber Pressure: 50.30 bar. Oxidizer to Fuel Ratio: 2.27.
Related
- Country
- USA
- Propellants
- Lox/Kerosene
- Agency
- Rocketdyne
- Bibliography
- 225