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RDMT-400
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Government Designation: 11D458. Designer: NII Mash. Application: Almaz, Kvant, Kristall, Spektr, Priroda. Propellants: N2O4/UDMH. Thrust(vac): 400 N (80 lbf). Isp: 255 sec. Mass Engine: 2.50 kg (5.50 lb). Chambers: 1. Chamber Pressure: 9.00 bar. Thrust to Weight Ratio: 16.40. Country: Russia. Status: In Production. Low-thrust attitude control thruster. Used in Isayev 11D458 engine.
Bibliography and Further Reading - Haeseler, Dietrich, Datasheets from NII Mashinostroeniye, Nishnaya Salda,
1992 via Dietrich Haeseler.
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