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Minotaur IV

Minotaur IV

Minotaur family · built by Orbital ATK · maiden flight 2010-09-26

Profile data last updated: 2026-08-15T20:08:04.839063+00:00 | 7531-09-01

The Minotaur IV 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.

Specifications

23.9 mLength
2.35 mDiameter
86 tLaunch mass
4Stages
2200 kNLiftoff thrust

Payload Capacity

1735 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.

5Total launches
5Successful
0Failed
1Upcoming

Launches Tracked on This Site

5In our archive
100.0%Success rate
Sep 26, 2010 04:41 UTCEarliest tracked
Apr 07, 2026 11:33 UTCMost recent
MissionDateStatus
Minotaur IV | STP-S29A Apr 07, 2026 11:33 UTC Success
Minotaur IV | NROL-174 Apr 16, 2025 19:33 UTC Success
Minotaur IV | NROL-129 Jul 15, 2020 13:46 UTC Success
Minotaur IV | ORS-5 Aug 26, 2017 06:04 UTC Success
Minotaur IV | SBSS (USA-216) Sep 26, 2010 04:41 UTC Success

Wikipedia