Juno II | S-45

Juno II

Family: Juno
Configuration:

Juno II was an American space launch vehicle used during the late 1950s and early 1960s. It was derived from the Jupiter missile, which was used as the first stage.

Specifications
  • Minimum Stage
    3
  • Max Stage
    4
  • Length
    24.0 m
  • Diameter
    2.67 m
  • Fairing Diameter
  • Launch Mass
    55 T
  • Thrust
    654 kN
Family
  • Name
    Juno II
  • Family
    Juno
  • Variant
  • Alias
  • Full Name
    Juno II
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    41 kg
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

Army Ballistic Missile Agency

Army Ballistic Missile Agency

(ABMA)

Successes: 1 Failures: 2 Pending: 0

Agency Type: Government

WIKI

Cape Canaveral, FL, USA

Pad: Space Launch Complex 26B


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