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Engine Model: 11D79. Government Designation: 11D79. Designer: Stepanov. Developed in: 1964-67. Application: Blok D SOZ. Propellants: N2O4/UDMH. Thrust(vac): 44.000 kN (9,891 lbf). Country: Russia. Status: In Production. Thrust 1.1-4.5 tf variable. 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. |