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R-7 Block I stage series
| Molniya 8K78-2 LOx/Kerosene propellant rocket stage. . |
 | R-9A Stage 2 LOx/Kerosene propellant rocket stage. Empty mass estimated. Developed into Molniya/Soyuz second stage. |
| Soyuz 11A511-2 LOx/Kerosene propellant rocket stage. . |
| Voskhod 11A57-2 LOx/Kerosene propellant rocket stage. . |
| Soyuz 11A511U2-2 LOx/Kerosene propellant rocket stage. . |
| 8K513 Blok B LOx/Kerosene propellant rocket stage. Masses estimated based on total vehicle mass of 117 metric tons. Developed into Molniya/Soyuz second stage. |
| Angara A-2 LOx/Kerosene propellant rocket stage. Two thrust levels. Propellant ration 2.6:1, chamber pressure 162 bar. |
| Molniya 8K78M-2 LOx/Kerosene propellant rocket stage. . |
| Soyuz 11A511U-2 LOx/Kerosene propellant rocket stage. . |
| Soyuz ST-2 LOx/Kerosene propellant rocket stage. . |
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