|
Government Designation: 11D445. Designer: Melnikov. Application: Yantar-2K descent propulsion. Propellants: N2O4/UDMH. Thrust(vac): 65 N (14 lbf). Burn time: 900 sec. Chambers: 1. Country: Russia. Status: In Production. Propulsion system of the Yantar-2K military satellite descent capsule. Up to 10,000 ignitions. Thrust from 0,065 - 0,012 kN.
Bibliography and Further Reading - Sorokin, Vladislav, Novosti Kosmonavtiki, "'Yantarnaya istoriya'", 1997, Issue 17, page 57.
|