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Minotaur IV HAPS

Orbital Sciences Corporation · Stati Uniti

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.

Costruttore
Orbital Sciences Corporation
Primo volo
20 novembre 2010
Lanci
1
Riusciti
1
Falliti
0
Altezza
23,9 m
Diametro
2,35 m
Massa al decollo
86 t
Carico in orbita bassa
1.750 kg
Riutilizzabile
no

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