S2.721V

Engine · Russia

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

Isayev Nitric acid/Amine rocket engine. KSR. Developed 1956-.

Chambers: 2. Thrust (sl): 6.860 kN (1,542 lbf). Thrust (sl): 700 kgf. Propellant Formulation: AK20F/TG-02.

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