Atlas G Centaur

In-active

Convair ()

June 9, 1984

Description

The Atlas G, also known as Atlas G Centaur-D1AR was an American expendable launch system derived from the Atlas-Centaur. It was a member of the Atlas family of rockets, and was used to launch seven communication satellites during the mid to late 1980s. Atlas G consisted of an improved Atlas core with modernized avionics and stretched propellant tanks. The Centaur stage also had several updated components and other technical improvements. It was replaced by the Atlas I, which had an improved guidance system.

Specifications
  • Stages
    2
  • Length
    38.0 m
  • Diameter
    3.05 m
  • Fairing Diameter
    3.05 m
  • Launch Mass
    166.0 T
  • Thrust
    1896.0 kN
Family
  • Name
    Atlas G Centaur
  • Family
  • Variant
    G Centaur
  • Alias
  • Full Name
    Atlas G Centaur
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    3630.0 kg
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

Convair

Commercial
None
1943

Convair, previously Consolidated Vultee, was an American aircraft manufacturing company that later expanded into rockets and spacecraft. The company was formed in 1943 by the merger of Consolidated Aircraft and Vultee Aircraft. In 1953 it was purchased by General Dynamics, and operated as their Convair Division for most of its corporate history.

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Mission:

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Cape Canaveral SFS, FL, USA
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Cape Canaveral SFS, FL, USA
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Mission:

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Cape Canaveral SFS, FL, USA
March 22, 1985, 11:55 p.m.
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Mission:

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Cape Canaveral SFS, FL, USA
June 9, 1984, 11:03 p.m.
Status: Launch Successful
Mission:

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