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8K513 Blok B

Stage · Russia

Original archive entry. The text, images and links below are kept as they were written.

LOx/Kerosene propellant rocket stage. Masses estimated based on total vehicle mass of 117 metric tons. Developed into Molniya/Soyuz second stage.

Country
Russia
Engines
NK-9V
Launch Vehicles
8K513
Propellants
Lox/Kerosene