Minotaur-C 2210
USA Wikipedia 
Built & Operated By
Orbital Sciences Corporation
Commercial
Family
Minotaur
variant 2210
Maiden Flight
10 FEB 1998
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.
Vehicle Specifications
Height
29.7 m
Diameter
2.35 m
Launch Mass
73 T
Thrust
1,380 kN
Stages
4
Configuration
Expendable
Launch Record
Total Launches
1
Successful
1
Failed
0
Consecutive
1
Performance
To LEO
1,380 kg