17D11
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Buran orientation engine
Credit: from Semenov, et. al., Buran, 1995.
Kosberg Lox/Kerosene rocket engine. Buran OMS and verniers. Out of Production. Buran orbital propulsion system, including 2 x 17D12, 38 x 17D15, 8 x RDMT-200K
Engine: 230 kg (500 lb). Chamber Pressure: 79.40 bar. Area Ratio: 189. Thrust to Weight Ratio: 38.26. Oxidizer to Fuel Ratio: 2.42.
Related
- Country
- Russia
- Propellants
- Lox/Kerosene
- Agency
- Korolev bureau