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R-3A stage

Stage · Russia

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

LOx/Alcohol propellant rocket stage. Further incremental upgrade of R-2. Payload 500 kg. Range 935 km. Developed from 1949 to October 1951. Cancelled, work combined with 8K14 development.

Country
Russia
Engines
RD-102
Launch Vehicles
R-3A
Propellants
Lox/Alcohol