Lockheed Martin

Atlas II

II

Retired

Overview

/01

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.

Manufacturer

Lockheed Martin

Variant

II

Alias

N/A

Maiden Flight

December 7, 1991

Technical Specifications

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47.54 m

Length

3.04 m

Diameter

0 t

Launch Mass

2479 kN

Liftoff Thrust

6580 kg

LEO Capacity

2810 kg

GTO Capacity

Launch Record

/03
10

Total Launches

10

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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