Minotaur family
Minotaur I
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 is built by Orbital Sciences Corporation of the United States. Company background, funding, contracts and news for this operator are tracked on Space Index. It first flew on 27 January 2000.
Flight record
Payload
| Low Earth orbit | 580kg |
|---|---|
| Sun-synchronous orbit | 331kg |
Vehicle
| Stages | 5 |
|---|---|
| Length | 19.21m |
| Diameter | 1.67m |
| Launch mass | 36t |
| Liftoff thrust | 935kN |
| Maiden flight | 2000-01-27 |
| Reusable | No |
Pads used
Orbits delivered
Launch history
| Date | Mission | Pad | Orbit | Outcome |
|---|---|---|---|---|
| 2021-06-15 | Minotaur I | NROL-111 | Launch Area 0 B | Low Earth Orbit | Success |
| 2013-11-20 | Minotaur I | ORS-3 | Launch Area 0 B | Low Earth Orbit | Success |
| 2011-06-30 | Minotaur I | ORS-1 (USA-231) | Launch Area 0 B | Low Earth Orbit | Success |
| 2011-02-06 | Minotaur I | NROL-66 (RPP) (USA-225) | Space Launch Complex 8 | Low Earth Orbit | Success |
| 2009-05-19 | Minotaur I | Tacsat 3 | Launch Area 0 B | Low Earth Orbit | Success |
| 2007-04-24 | Minotaur I | NFIRE | Launch Area 0 B | Low Earth Orbit | Success |
| 2006-12-16 | Minotaur I | Tacsat 2 | Launch Area 0 B | Low Earth Orbit | Success |
| 2006-04-15 | Minotaur I | COSMIC 1-6 | Space Launch Complex 8 | Low Earth Orbit | Success |
| 2005-09-23 | Minotaur I | STP-R1 | Space Launch Complex 8 | Low Earth Orbit | Success |
| 2005-04-11 | Minotaur I | XSS-11 | Space Launch Complex 8 | Low Earth Orbit | Success |
| 2000-07-19 | Minotaur I | Sindri | Space Launch Complex 8 | Polar Orbit | Success |
| 2000-01-27 | Minotaur I | JAWSAT & FalconSat 1 | Space Launch Complex 8 | Low Earth Orbit | Success |
Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.
Further reading: Wikipedia