Proton / UR-500 K/D | Soyuz 7K-L1E No.1

Proton

Family: Proton / UR-500
Configuration: K/D

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

Specifications
  • Stages
    4
  • Length
    57.0 m
  • Diameter
    4.0 m
  • Fairing Diameter
  • Launch Mass
    696 T
  • Thrust
    8847 kN
Family
  • Name
    Proton
  • Family
    Proton / UR-500
  • Variant
    K/D
  • Alias
  • Full Name
    Proton / UR-500 K/D
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

Soyuz 7K-L1E No.1


Active Human Rated Unmanned Crew Capacity: 3
Destination: Low Earth Orbit
Serial Number: Soyuz 7K-L1E

The Soyuz 7K-L1 "Zond" spacecraft was designed to launch men from the Earth to circle the Moon without going into lunar orbit in the context of the Soviet crewed Moon-flyby program in the Moon race. It was based on the Soyuz 7K-OK.

Soyuz Details

Russian Federal Space Agency (ROSCOSMOS)

Circle Image
Administrator: Yuri Borisov Founded: 1992 Successes: 297 Failures: 11 Pending: 9

Agency Type: Government

The Roscosmos State Corporation for Space Activities, commonly known as Roscosmos, is the governmental body responsible for the space science program of the Russian Federation and general aerospace research. Soyuz has many launch locations the Russian sites are Baikonur, Plesetsk and Vostochny however Ariane also purchases the vehicle and launches it from French Guiana.

INFO WIKI

Baikonur Cosmodrome, Republic of Kazakhstan

81/23 (81L)


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