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Designer: Kosberg. Developed in: 1956. Application: Missile by Toropov. Propellants: Isopropylnitrate Thrust(vac): 1,203 kgf. Thrust(vac): 11.80 kN. Isp (sea level): 200 sec. Burn time: 6 sec. Chambers: 1. Chamber Pressure: 29.40 bar. Country: Russia. Status: Out of Production. References: 309 . Comments: Intended for air-air missile by I I Toropov. Uncooled thrust chamber. Sea level thrust 11.8 kN.
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Last update 12 March 2001.
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© Mark Wade, 2001 .