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Isayev P-15
Isayev Nitric acid/Amine rocket engine. P-15 Termit. Out of Production. Designation unknown. Thrust range 11.895-5.43 kN.

Status: Out of Production. Date: 1955-60. Thrust: 11.90 kN (2,675 lbf).

Throttled thrust(vac): 5.430 kN (1,221 lbf). Thrust (sl): 5.432 kN (1,221 lbf). Thrust (sl): 554 kgf. Propellant Formulation: AK20K/TG-02.



Family: Storable liquid. Country: Russia. Propellants: Nitric acid/Amine. Agency: Isayev bureau. Bibliography: 342, 344.

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