Description
American all-solid orbital launch vehicle based on a Pegasus and Peacekeeper rocket.It has been designed as a quick reaction launch vehicle, which can be launched from minimaly prepared places in a matter of a few days.
Specifications
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Stages
4
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Length
31.6 m
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Diameter
2.35 m
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Fairing Diameter
2.35 m
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Launch Mass
73.0 T
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Thrust
1380.0 kN
Family
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Name
Minotaur-C 3110
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Family
―
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Variant
3110
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Alias
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Full Name
Minotaur-C 3110
Payload Capacity
-
Launch Cost
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Low Earth Orbit
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Geostationary Transfer
Orbit
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Direct Geostationary
―
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Sun-Synchronous Capacity
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