Minotaur IV+ (Orbital Sciences Corporation)
The Minotaur IV+ is a non-reusable, active launch vehicle manufactured by Orbital Sciences Corporation. It undertook its inaugural launch on 09/27/2011.
The Minotaur IV+ launch system is derived from the Peacekeeper ICBM. The first three stages are taken directly from decommissioned Peacekeeper missiles. It is similar to the Minotaur IV, but uses a larger Star-48V upper stage in place of the Orion-38 used on the baseline Minotaur IV.
Minotaur IV+ Specifications
| Variant | + |
|---|---|
| Alias | Peacekeeper SLV |
| Length | 23.9 m |
| Diameter | 2.35 m |
| Stages | 4 |
| Launch Mass | 86 T |
| Takeoff Thrust | 2200 kN |
| Apogee | 500 km |
| LEO Capacity | 1950 kg |
Minotaur IV+ Launch Record
| Total Launches | 1 |
|---|---|
| Successful Launches | 1 |
| Consecutive Successful Launches | 1 |