Chemical Automatics Design Bureau - Notable Engine Designs

Notable Engine Designs

Engine Other Designations Thermodynamic Cycle Thrust, kN (vacuum) Specific Impulse, s (vacuum) Propellants Engine Mass, kg Development period Notes
RD-0110 11D55, RD-461 Gas Generator 298 326 LOX/Kerosene 408 1963–1967 Soyuz, Molniya, 3rd stage,
RD-0120 11D122, RO-200 Staged Combustion 1962 455 LOX/LH2 3450 1967–1983 Energia, core,
RD-0124 14D451M, 14D23 Staged Combustion 294 359 LOX/Kerosene 450 1996–1999 Soyuz, 3rd stage,
RD-0146 Expander 98 451 LOX/LH2 242 2000- Replacement for the RL10A-4-1,
RD-0210 8D411K, RD-465, 8D49 Staged Combustion 598 326 N2O4/UDMH 565 1963–1967 Proton, 2nd stage
RD-0410 11B91 Expander 35.3 910 Nuclear/LH2 2000 1965–1994 The only operational nuclear engine in the USSR/Russia,
RD-0243 Staged Combustion 825 300 N2O4/UDMH 853 1977–1985 SS-N-23 submarine-launched ballistic missile,

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