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RDMT-200K
Part of RDMT engine series Family
NII Mash GOX/Kerosene rocket engine. Buran. Out of Production. Low-thrust attitude control thruster. Mass in ref. NIIMash 95 given as only 2.5 kg.

Status: Out of Production. Thrust: 200 N (40 lbf). Unfuelled mass: 5.50 kg (12.10 lb). Specific impulse: 265 s.

Engine: 5.50 kg (12.10 lb). Thrust to Weight Ratio: 3.63.



Country: Russia. Propellants: GOX/Kerosene. Agency: NII Mash. Bibliography: 336.

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