RD-58MF
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg Lox/Kerosene rocket engine. In Production. Multi-function variant of RD-58 for uprated upper stages applications (Zenit stage 3, Angara). Block-DM-SL for Sea-Launch may have used RD-58M.
Also proposed for N12RA, Proryv, LM, 315GK for Zenit, Angara, Energia-M.
Engine: 230 kg (500 lb). Chamber Pressure: 77.50 bar. Area Ratio: 189. Thrust to Weight Ratio: 36.95.
Related
- Country
- Russia
- Propellants
- Lox/Kerosene
- Agency
- Korolev bureau