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RDMT-0.8
Part of RDMT engine series Family
Status: In Production. Thrust: 0.80 N (0.17 lbf). Unfuelled mass: 0.10 kg (0.22 lb). Specific impulse: 70 s.

Engine: 0.10 kg (0.22 lb). Thrust to Weight Ratio: .81.



Family: Cold Gas. Country: Russia. Propellants: Nitrogen+Helium. Agency: NII Mash. Bibliography: 336.

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