Isayev V-750V

Engine · Russia

Original archive entry. The text, images and links below are kept as they were written.

Isayev Nitric acid/Amine rocket engine. SAM-missile V-750V. Out of Production. Designation unknown.

Engine: 43 kg (94 lb). Propellant Formulation: AK20K/TG-02. Thrust to Weight Ratio: 72.09.

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