Minotaur-C 2210 (Orbital Sciences Corporation)
The Minotaur-C 2210, manufactured by Orbital Sciences Corporation established in unknown year, undertook its inaugural launch on 02/10/1998, is non-reusable and is active.
Minotaur-C 2210 has 1 successful launches and 0 failed attempts, with a cumulative tally of 1 launches, currently with 0 pending launches in the pipeline.
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.
- Length: 29.7 m
- Diameter: 2.35 m
- Launch Mass: 73 T
- LEO Capacity: 1380 kg
