Minotaur-C 2210
OSC
Details
Height
29.7 m
Diameter
2.35 m
GTO
Unknown
LEO
1,380 kg
Thrust at Liftoff
1,380 kN
Apogee
Unknown
Launch Cost
Unknown
Maiden Flight
February 10, 1998
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.