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RDMT-2600
Part of RDMT engine series Family
NII Mash GOX/Alcohol rocket engine. Developed 1980's. Experimental low-thrust thruster.

Status: Developed 1980's. Thrust: 2.60 kN (585 lbf). Unfuelled mass: 5.00 kg (11.00 lb). Specific impulse: 270 s.

Engine: 5.00 kg (11.00 lb). Thrust to Weight Ratio: 53.



Country: Russia. Propellants: GOX/Alcohol. Agency: NII Mash. Bibliography: 336.

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