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RDMT-8 X
Part of RDMT engine series Family
NII Mash N2O4/UDMH rocket engine. Developed 1980's. Experimental low-thrust thruster.

Status: Developed 1980's. Thrust: 8.00 N (1.70 lbf). Unfuelled mass: 0.0250 kg (0.0550 lb). Specific impulse: 296 s.

Engine: 0.0250 kg (0.0550 lb). Chamber Pressure: 30.00 bar. Thrust to Weight Ratio: 32.79.



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

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