RDMT-135

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RDMT-135

Part of RDMT engine series

NII Mash N2O4/UDMH rocket engine. Salyut, Mir, Soyuz-T and -TM, Progress, Kosmos-satellites. In Production. Low-thrust attitude control thruster.

Status: In Production. Thrust: 135 N (30 lbf). Unfuelled mass: 1.20 kg (2.60 lb). Specific impulse: 260 s.

Engine: 1.20 kg (2.60 lb). Chamber Pressure: 9.00 bar. Thrust to Weight Ratio: 11.66.

Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Agency: NII Mash. Bibliography: 336, 7529.

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