Minotaur I (Orbital Sciences Corporation)
The Minotaur I is a non-reusable, active launch vehicle manufactured by Orbital Sciences Corporation. It undertook its inaugural launch on 01/27/2000.
The Minotaur I launch system is derived from converted Minuteman II ICBMs and is used to launch small satellites for the US Government. The first and second stages, taken directly from decommissioned Minuteman missiles, are mated to the Orion third and fourth stages taken from the Pegasus XL air-launched rocket family. An optional hydrazine-powered fifth stage called HAPS can be used.The Minotaur I launch system is derived from converted Minuteman II ICBMs and is used to launch small satellites for the US Government. An optional hydrazine-powered fifth stage called HAPS can be used.
Minotaur I Specifications
| Alias | Minotaur OSP-SLV |
|---|---|
| Length | 19.21 m |
| Diameter | 1.67 m |
| Stages | 4-5 |
| Launch Mass | 36 T |
| Takeoff Thrust | 935 kN |
| LEO Capacity | 580 kg |
| SSO Capacity | 331 kg |
Minotaur I Launch Record
| Total Launches | 12 |
|---|---|
| Successful Launches | 12 |
| Consecutive Successful Launches | 12 |