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Engine Model: D-7. Designer: Kosberg. Developed in: 1956. Application: Missile by Toropov. Propellants: Isopropylnitrate. Thrust(vac): 11.800 kN (2,653 lbf). Isp (sea level): 200 sec. Burn time: 6.00 sec. Chambers: 1. Chamber Pressure: 29.40 bar. Country: Russia. Status: Out of Production.

Intended for air-air missile by I I Toropov. Uncooled thrust chamber. Sea level thrust 11.8 kN.

Bibliography:

  • Golubev, A A, KB KhimAvtomatiki - Straniy Istorii, Vol. 1, Voronezh 1995 via Dietrich Haeseler.
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