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RDMT-0.4 X
Part of RDMT engine series Family
NII Mash N2O4/UDMH rocket engine. In Production. Experimental low-thrust thruster. Chamber from niobium alloy. Chamber pressure 41 / 17 bar. Specific impulse 313 / 302,3 sec.

Status: In Production. Thrust: 0.40 N (0.08 lbf). Unfuelled mass: 0.10 kg (0.22 lb). Specific impulse: 290 s.

Engine: 0.10 kg (0.22 lb). Chamber Pressure: 41.00 bar. Thrust to Weight Ratio: .4.



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

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