Fuel: Isopropylnitrate.
Propellant Formulation: OT-152.
More... - Chronology...
Associated Engines
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D-1 Kosberg isopropylnitrate monopropellant rocket engine. 39 kN. Developed 1955-56. Second thrust level at 50%. Explosion of D-1 on test bench in 1956 forced stop of work with mono-propellant OT-152. Sea level thrust 39 kN. More...
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D-7 Kosberg isopropylnitrate monopropellant rocket engine. 11.8 kN. Missile by Toropov. Out of Production. Intended for air-air missile by I I Toropov. Uncooled thrust chamber. Sea level thrust 11.8 kN. More...
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Hustler APU Aerojet isopropylnitrate monopropellant rocket engine. B-58. Development begun 1953. APU for the Hustler 'controlled bomb pod', which was really a long range air to surface strategic missile More...
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XCNLT-1500 Aerojet isopropylnitrate monopropellant rocket engine. Lark. Launch thrust 6.66 kN. Development begun March 1945. Turborocket; turbine-pump fed monopropellant, single uncooled thrust chamber. Development unsuccessful, all work terminated. More...
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