S2.145 Other Designations: S2.145. Designer: Isayev. Developed in: 1950s early. Thrust(vac): 88.000 kN (19,783 lbf). Country: Russia. Status: Developed 1950s early.                   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.

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