Vehicle / SINCE 2010

Minotaur IV

ABOUT

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 10
Length 23.9 m
Diameter 2.35 m
Launch Mass T 86
Leo Capacity 1,750 kg
Gto Capacity 0 kg
Thrust 2,200 kN
Reusable No
Total Launches 1
Successful Launches 1
Maiden Flight 2010-11-20