This page no longer updated from 31 October 2001. Latest version can be found at RDMT-200K

Designer: NII Mash. Application: Buran. Propellants: GOX/Kerosene Thrust(vac): 20 kgf. Thrust(vac): 0.20 kN. Isp: 265 sec. Mass Engine: 6 kg. Chambers: 1. Country: Russia. Status: Out of Production. References: 336 . Comments: Low-thrust attitude control thruster. Mass in ref. NIIMash 95 given as only 2.5 kg.
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Last update 12 March 2001.
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© Mark Wade, 2001 .