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Engine Model: RDMT-200. Designer: NII Mash. Application: Almaz. Propellants: N2O4/UDMH. Thrust(vac): 200 N (40 lbf). Isp: 255 sec. Mass Engine: 2.00 kg (4.40 lb). Chambers: 1. Chamber Pressure: 9.00 bar. Thrust to Weight Ratio: 10.00. Country: Russia. Status: In Production.

Low-thrust attitude control thruster.

Engine Model: RDMT-200K. 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:

  • Haeseler, Dietrich, Datasheets from NII Mashinostroeniye, Nishnaya Salda, 1992 via Dietrich Haeseler.
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