This page no longer updated from 31 October 2001. Latest version can be found at Izotov UR-100 stage 2 vernier

Designer: Izotov. Developed in: 1963-67. Application: UR-100 stage II vernier. Used on stages: UR-100 Stage 2. Used on launch vehicles: UR-100. Propellants: N2O4/UDMH Thrust(vac): 6,000 kgf. Thrust(vac): 58.00 kN. Chambers: 4. Country: Russia. Status: Out of Production.
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Last update 12 March 2001.
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© Mark Wade, 2001 .