RD-0250
Manufacturer Name: RD-0250. Designer: Kosberg. Application: Modif. of Chelomei-launcher stage 2 (?). Propellants: N2O4/UDMH. Chambers: 1. Country: Russia. Status: Design concept.

Further development of RD-0235 main engine for projected modification of launcher by Chelomei. Development ceased during study phase. Staged combustion cycle.


Bibliography and Further Reading
  • Golubev, A A, KB KhimAvtomatiki - Straniy Istorii, Vol. 1, Voronezh 1995 via Dietrich Haeseler.
 
 
 
 
 
 
 
 
 

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