S09.502

Designer: Isayev. Developed in: May 1949. Application: R-101 SAM. Propellants: Nitric acid/Amine. Thrust(sl): 78.400 kN (17,625 lbf). Chambers: 4. Country: Russia. Status: Developed 1949-50.

Four chamber engine designed for use in the R-101 (derivative of German Wasserfall). Abandoned by 1950 in favour of single-chamber engine.

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 - 2007 except where otherwise noted.

Encyclopedia Astronautica
topic index
0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z