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
Description
This four stage version of the Proton was originally designed to send manned circumlunar spacecraft into translunar trajectory.