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Proton / UR-500 K/D
RFSA
Details
Height
57 m
Diameter
4 m
GTO
Unknown
LEO
Unknown
Thrust at Liftoff
8,847 kN
Apogee
Unknown
Launch Cost
Unknown
Maiden Flight
March 10, 1967
Statistics
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Description
This four stage version of the Proton was originally designed to send manned circumlunar spacecraft into translunar trajectory.
Agency
Russian Federal Space Agency
RFSA
Links
Wikipedia
en.wikipedia.org