Minotaur V
USA Wikipedia 
Built & Operated By
Orbital Sciences Corporation
Commercial
Family
Minotaur
Maiden Flight
7 SEP 2013
Vehicle Specifications
Height
23.9 m
Diameter
2.35 m
Launch Mass
36 T
Thrust
1,600 kN
Stages
1–5
Configuration
Expendable
Launch Record
Total Launches
1
Successful
1
Failed
0
Consecutive
1
Performance
To LEO
1,735 kg
Apogee
500 km