Atlas IIA
In-activeLockheed Martin (LMT)
June 10, 1992
Description
Atlas II was a member of the Atlas family of launch vehicles, which evolved from the successful Atlas missile program of the 1950s. It was designed to launch payloads into low earth orbit, geosynchronous transfer orbit or geosynchronous orbit. Sixty-three launches of the Atlas II, IIA and IIAS models were carried out between 1991 and 2004; all sixty-three launches were successes, making the Atlas II the most reliable launch system in history.
Specifications
-
Stages
3 -
Length
47.54 m -
Diameter
3.04 m -
Fairing Diameter
3.04 m -
Launch Mass
204.0 T -
Thrust
2479.0 kN
Family
-
Name
Atlas IIA -
Family
― -
Variant
IIA -
Alias
― -
Full Name
Atlas IIA
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
6580.0 kg -
Geostationary Transfer
Orbit
2810.0 kg -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
Lockheed Martin
Commercial
None
LMT 1953Lockheed Martin's Space Division started in the production of missiles and later ICBM's in the 1950s. Their TITAN missile system was used for 12 Gemini spacecraft and the Voyager probes. They have worked largely in collaboration with NASA on many of their probes, landers, and spacecraft, and hope to play a key role in NASA's return to the moon in 2024.
Flight Record
No spaceflights found for .
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