Orbital Sciences Corporation
Minotaur IV HAPS
HAPS

Active
Overview
/01The 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.
Manufacturer
Orbital Sciences Corporation
Variant
HAPS
Alias
Peacekeeper SLV
Maiden Flight
November 20, 2010
Technical Specifications
/0223.9 m
Length
2.35 m
Diameter
0 t
Launch Mass
2200 kN
Liftoff Thrust
1750 kg
LEO Capacity
0 kg
GTO Capacity
Launch Record
/031
Total Launches
1
Successful
0
Failed
100.0%
Success Rate
0
Attempted Landings
0
Successful Landings
0
Failed Landings
0
Consecutive Successes