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Space · launch vehicle

Minotaur IV

OA ACTIVE
At a glance
Launches
5
1 pending
Success rate
100%
5 ok · 0 failed
Payload to LEO
1,735 kg
Payload to GTO
0 kg
Manufacturer
Orbital ATK
Status
Active
First flight
26 Sept 2010
Reusable
No
Height
23.9 m
Diameter
2.35 m
Launch mass
86 t
Liftoff thrust
2,200 kN
Stages
4
Launch cost
—
Booster landings
—
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About

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.