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The Atlas I was a US expendable launch system manufactured by General Dynamics in the 1990s to launch a variety of satellites. Though the Atlas I was marketed as a new rocket, it was mostly a re-brand of the Atlas G/H for commercial payloads. The Atlas G and H launched mostly governmental satellites. Atlas I was the last use of the classic Atlas design with three engines, a jettisonable booster section, and two vernier engines. Atlas II, while retaining most of those features, replaced the verniers with a hydrazine roll control system.
Missions
11
Success Rate
72.7%
Successes
8
Failures
3
Success Streak
6
Partial Failures
0
Active 1990 to 1997
Rocket
Height: 43.9m
Stages
2