Minotaur-C 1110 (Orbital Sciences Corporation)
The Minotaur-C 1110 is a non-reusable, active launch vehicle manufactured by Orbital Sciences Corporation. It undertook its inaugural launch on 03/12/2000.
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 1110 Specifications
| Variant | 1110 |
|---|---|
| Length | 27.9 m |
| Diameter | 2.35 m |
| Stages | 4 |
| Launch Mass | 73 T |
| Takeoff Thrust | 1320 kN |
| LEO Capacity | 1320 kg |
Minotaur-C 1110 Launch Record
| Total Launches | 1 |
|---|---|
| Successful Launches | 1 |
| Consecutive Successful Launches | 1 |
Manufacturer
Orbital Sciences Corporation (OSC)