This page no longer updated from 31 October 2001. Latest version can be found at 11D445

Government Designation: 11D445. Designer: Melnikov. Application: Yantar-2K descent propulsion. Used on spacecraft: Yantar-2K. Propellants: N2O4/UDMH Thrust(vac): 7 kgf. Thrust(vac): 0.07 kN. Burn time: 900 sec. Chambers: 1. Country: Russia. Status: In Production. References: 69 . Comments: Propulsion system of the Yantar-2K military satellite descent capsule. Up to 10,000 ignitions. Thrust from 0,065 - 0,012 kN.
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Last update 12 March 2001.
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© Mark Wade, 2001 .