Isayev P-15
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev Nitric acid/Amine rocket engine. P-15 Termit. Out of Production. Designation unknown. Thrust range 11.895-5.43 kN.
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.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- Nitric acid/Amine
- Agency
- Isayev bureau