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S2.721V
Isayev Nitric acid/Amine rocket engine. KSR. Developed 1956-.

AKA: S2.721. Status: Developed 1956-. Date: 1956-. Thrust: 11.80 kN (2,653 lbf).

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

Family: Storable liquid. Country: Russia. Propellants: Nitric acid/Amine. Agency: Isayev bureau.
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