Isayev P-15

Isayev P-15

home
topic index

Engine Model: Isayev P-15. Designer: Isayev. Developed in: 1955-60. Application: P-15 Termit. Propellants: Nitric acid/Amine. Thrust(vac): 11.900 kN (2,675 lbf). Thrust(sl): 5.432 kN (1,221 lbf). Throttled thrust(vac): 5.430 kN (1,221 lbf). Chambers: 1. Country: Russia. Status: Out of Production.

Designation unknown. Thrust range 11.895-5.43 kN.

Bibliography:

Russian Arms Catalogue, Vol 5 and 6, Military Parade, Moscow via Dietrich Haeseler.

Siddiqi, Asif A, Soviet Space Web Page, 1999 via Dietrich Haeseler. Web Address when accessed: http://home.earthlink.net/~cliched/main_space.html.

Contact us with any corrections, additions, or comments.

Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.

© Mark Wade, 1997 - 2008 except where otherwise noted.