RDMT-400A (original) (raw)

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RDMT-400A

Part of RDMT engine series

NII Mash N2O4/UDMH rocket engine. Developed 1980's. Experimental low-thrust thruster. Niobium combustion chamber with coating.

Status: Developed 1980's. Thrust: 400 N (80 lbf). Unfuelled mass: 2.80 kg (6.10 lb). Specific impulse: 290 s.

Engine: 2.80 kg (6.10 lb). Thrust to Weight Ratio: 14.64.

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

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