Minotaur IV HAPS
Minotaur family
· built by Orbital Sciences Corporation
· maiden flight 2010-11-20
Profile data last updated: 2026-08-29T15:37:07.354998+00:00 | 7531-10-17
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.
Specifications
23.9 mLength
2.35 mDiameter
86 tLaunch mass
5Stages
2200 kNLiftoff thrust
Payload Capacity
1750 kgTo LEO
Lifetime Launch Record
As reported by Launch Library 2 across this rocket's entire history, not just the launches tracked on this site.
1Total launches
1Successful
0Failed
0Upcoming
Launches Tracked on This Site
1In our archive
100.0%Success rate
Nov 20, 2010 01:25 UTCEarliest tracked
Nov 20, 2010 01:25 UTCMost recent
| Mission | Date | Status |
|---|---|---|
| Minotaur IV HAPS | STP S-26 | Nov 20, 2010 01:25 UTC | Success |