Minotaur-C 2210 (Orbital Sciences Corporation)
The Minotaur-C 2210 is a non-reusable, active launch vehicle manufactured by Orbital Sciences Corporation. It undertook its inaugural launch on 02/10/1998.
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.
Minotaur-C 2210 Specifications
| Variant | 2210 |
|---|---|
| Length | 29.7 m |
| Diameter | 2.35 m |
| Stages | 4 |
| Launch Mass | 73 T |
| Takeoff Thrust | 1380 kN |
| LEO Capacity | 1380 kg |
Minotaur-C 2210 Launch Record
| Total Launches | 1 |
|---|---|
| Successful Launches | 1 |
| Consecutive Successful Launches | 1 |
Manufacturer
Orbital Sciences Corporation (OSC)