Russian Federal Space Agency (ROSCOSMOS)

Proton / UR-500 K/D

K/D

Proton / UR-500 K/D
Retired

Overview

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

Manufacturer

Russian Federal Space Agency (ROSCOSMOS)

Variant

K/D

Alias

N/A

Maiden Flight

March 10, 1967

Technical Specifications

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57 m

Length

4 m

Diameter

1 t

Launch Mass

8847 kN

Liftoff Thrust

LEO Capacity

GTO Capacity

Launch Record

/03
39

Total Launches

24

Successful

15

Failed

61.5%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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