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, |
Read more about this topic: Chemical Automatics Design Bureau
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