Izotov UR-100 stage 2 vernier

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Engine Model: Izotov UR-100 stage 2 vernier. Designer: Izotov. Developed in: 1963-67. Application: UR-100 stage II vernier. Propellants: N2O4/UDMH. Thrust(vac): 58.000 kN (13,038 lbf). Chambers: 4. Country: Russia. Status: Out of Production. 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.