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Space · launch vehicle

Minotaur-C 2210

OSC ACTIVE
At a glance
Launches
1
Success rate
100%
1 ok · 0 failed
Payload to LEO
1,380 kg
Payload to GTO
—
Status
Active
First flight
10 Feb 1998
Reusable
No
Height
29.7 m
Diameter
2.35 m
Launch mass
73 t
Liftoff thrust
1,380 kN
Stages
4
Launch cost
—
Booster landings
—
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Next flight
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About

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.