17D11
Buran RCS
Credit - from Semenov, et. al., Buran, 1995.
Government Designation: 17D11. Designer: Korolev. Developed in: 1976-88. Application: Buran OMS and verniers. Propellants: Lox/Kerosene. Thrust(vac): 86.300 kN (19,401 lbf). Isp: 362 sec. Burn time: 680 sec. Mass Engine: 230 kg (500 lb). Diameter: 1.17 m (3.83 ft). Length: 2.27 m (7.44 ft). Chambers: 1. Chamber Pressure: 79.40 bar. Area Ratio: 189.00. Oxidizer to Fuel Ratio: 2.42. Thrust to Weight Ratio: 38.26. Country: Russia. Status: Out of Production.

Buran orbital propulsion system, including 2 x 17D12, 38 x 17D15, 8 x RDMT-200K

Bibliography and Further Reading
  • Haeseler, Dietrich, Information from NPO Energia museum exhibit, Nov. 1992 via Dietrich Haeseler.
  • Burya article, Lavochkin web site.
 
 
 
 
 
 
 
 
 
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