This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: NII Mash. Application: MMK. Propellants: Air Thrust(vac): 1 kgf. Thrust(vac): 0.01 kN. Isp: 70 sec. Mass Engine: 0 kg. Chambers: 1. Country: Russia. Status: In Production. References: 336 . Comments: Low-thrust cold-gas thruster.
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Last update 12 March 2001.
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© Mark Wade, 2001 .