D-7

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D-7

Part of D-1

Kosberg isopropyl nitrate monopropellant rocket engine. Missile by Toropov. Out of Production. Intended for air-air missile by I I Toropov. Uncooled thrust chamber. Sea level thrust 11.8 kN.

Status: Out of Production. Date: 1956. Thrust: 11.80 kN (2,653 lbf). Specific impulse: 200 s. Specific impulse sea level: 200 s. Burn time: 6.00 s.

Chamber Pressure: 29.40 bar. Propellant Formulation: OT-152.

Family: Monopropellant. Country: Russia. Propellants: Isopropylnitrate. Agency: Kosberg bureau. Bibliography: 309.

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