ORBITAL 轨道桥
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Rockets / Lockheed Martin

Atlas IIA

Atlas IIA · Lockheed Martin · retired

Total launches
23
all time
Success rate
0.0%
23 of 23
Failed
0
all time
Pending
0
0 on the board
About this vehicle

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.

Source: Launch Library 2 record #254 · Wikipedia

Specifications
Manufacturer
Lockheed Martin
Status
Retired / inactive
Reusable
No
Maiden flight
1992-06-10
Height
47.5 m
Diameter
3.0 m
Liftoff mass
204 t
Thrust
2,479 kN
Stages
3
Payload to LEO
6,580 kg
Payload to GTO
2,810 kg
Launch cost
—

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