RD-120M
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko LOx/Kerosene rocket engine. PacAstro-2 stage 1. Out of Production. Sea-level variant of RD-120 engine, similar to RD-120K. Gimbaling +/- 6 degree in two planes.
Engine: 1,080 kg (2,380 lb). Chamber Pressure: 176.30 bar. Area Ratio: 4.96. Thrust to Weight Ratio: 80.29. Oxidizer to Fuel Ratio: 2.6.
Related
- Country
- Russia
- Propellants
- Lox/Kerosene
- Agency
- Glushko bureau