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Minotaur-C 3110
OSC
Details
Height
31.6 m
Diameter
2.35 m
GTO
Unknown
LEO
Unknown
Thrust at Liftoff
1,380 kN
Apogee
Unknown
Launch Cost
Unknown
Maiden Flight
February 24, 2009
Statistics
Pro
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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.
Agency
Orbital Sciences Corporation
OSC
Links
Wikipedia
en.wikipedia.org