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RDMT-200
Part of RDMT engine series Family
NII Mash N2O4/UDMH rocket engine. Almaz. In Production. Low-thrust attitude control thruster.

Status: In Production. Thrust: 200 N (40 lbf). Unfuelled mass: 2.00 kg (4.40 lb). Specific impulse: 255 s.

Engine: 2.00 kg (4.40 lb). Chamber Pressure: 9.00 bar. Thrust to Weight Ratio: 10.



Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Agency: NII Mash. Bibliography: 336.

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