S-155
Designer: Dushkin. Developed in: 1955-56. Application: E-50. Thrust(vac): 39.000 kN (8,767 lbf). Country: Russia. Status: Developed 1955-56.

Thrust variable 2000 - 4000 kgf.  
 
 
 
 
 
 
 
 

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