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Space · launch vehicle

Minotaur IV+

OSC ACTIVE
At a glance
Launches
1
Success rate
100%
1 ok · 0 failed
Payload to LEO
1,950 kg
Payload to GTO
0 kg
Status
Active
First flight
27 Sept 2011
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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Next flight
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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. It is similar to the Minotaur IV, but uses a larger Star-48V upper stage in place of the Orion-38 used on the baseline Minotaur IV.