Minotaur IV HAPS (Orbital Sciences Corporation)
The Minotaur IV HAPS is a non-reusable, active launch vehicle manufactured by Orbital Sciences Corporation. It undertook its inaugural launch on 11/20/2010.
The Minotaur IV HAPS launch system is derived from the Peacekeeper ICBM. The first three stages are taken directly from decommissioned Peacekeeper missiles. A fourth stage, the Orion-38, is taken from the Pegasus family of air-launched rockets. A fifth stage, consisting of a hydrazine-powered motor called HAPS, increases orbital insertion accuracy and allows additional orbital maneuvering.
Minotaur IV HAPS Specifications
| Variant | HAPS |
|---|---|
| Alias | Peacekeeper SLV |
| Length | 23.9 m |
| Diameter | 2.35 m |
| Stages | 5 |
| Launch Mass | 86 T |
| Takeoff Thrust | 2200 kN |
| Apogee | 500 km |
| LEO Capacity | 1750 kg |
Minotaur IV HAPS Launch Record
| Total Launches | 1 |
|---|---|
| Successful Launches | 1 |
| Consecutive Successful Launches | 1 |