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.