Family:
Configuration: I
The Atlas I was a US expendable launch system manufactured by General Dynamics in the 1990s to launch a variety of satellites.
Specifications
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Stages
2
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Length
43.9 m
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Diameter
3.05 m
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Fairing Diameter
3.05 m
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Launch Mass
164.0 T
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Thrust
1939.0 kN
Family
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Name
Atlas I
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Family
―
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Variant
I
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Alias
―
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Full Name
Atlas I
Payload Capacity
-
Launch Cost
―
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Low Earth Orbit
5900.0 kg
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Geostationary Transfer
Orbit
―
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Direct Geostationary
―
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Sun-Synchronous Capacity
―