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RDMT-200K
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Designer: NII Mash. Application: Buran. Propellants: GOX/Kerosene. Thrust(vac): 200 N (40 lbf). Isp: 265 sec. Mass Engine: 5.50 kg (12.10 lb). Chambers: 1. Thrust to Weight Ratio: 3.63. Country: Russia. Status: Out of Production. Low-thrust attitude control thruster. Mass in ref. NIIMash 95 given as only 2.5 kg.
Bibliography and Further Reading - Haeseler, Dietrich, Datasheets from NII Mashinostroeniye, Nishnaya Salda,
1992 via Dietrich Haeseler.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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