This page no longer updated from 31 October 2001. Latest version can be found at RDMT-2600

Designer: NII Mash. Propellants: GOX/Alcohol Thrust(vac): 265 kgf. Thrust(vac): 2.60 kN. Isp: 270 sec. Mass Engine: 5 kg. Chambers: 1. Country: Russia. Status: Developed 1980's. References: 336 . Comments: Experimental low-thrust thruster.
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Last update 12 March 2001.
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© Mark Wade, 2001 .