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Minotaur IV HAPS (Orbital Sciences Corporation)

Minotaur IV
Photo Credit: USAF

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

Technical specifications for Minotaur IV HAPS
VariantHAPS
AliasPeacekeeper SLV
Length23.9 m
Diameter2.35 m
Stages5
Launch Mass86 T
Takeoff Thrust2200 kN
Apogee500 km
LEO Capacity1750 kg

Minotaur IV HAPS Launch Record

Launch statistics for Minotaur IV HAPS
Total Launches1
Successful Launches1
Consecutive Successful Launches1

Manufacturer

Orbital Sciences Corporation (OSC)
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