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Designer: NII Mash. Propellants: N2O4/UDMH Thrust(vac): 41 kgf. Thrust(vac): 0.40 kN. Isp: 296 sec. Mass Engine: 0 kg. Chambers: 1. Chamber Pressure: 30.00 bar. Country: Russia. Status: Developed 1980's. References: 336 . Comments: Experimental low-thrust thruster. Carbon combustion chamber. Mass may be chamber only.
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Last update 12 March 2001.
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© Mark Wade, 2001 .