🚀Launchpad

Minotaur I

Orbital Sciences Corporation

Hersteller
Orbital Sciences Corporation
Familie
Minotaur
Erstflug
2000-01-27
Länge
19.21 m
Durchmesser
1.67 m
Nutzlast LEO
580 kg
Starts
12
Erfolgreich
12

The Minotaur I launch system is derived from converted Minuteman II ICBMs and is used to launch small satellites for the US Government. The first and second stages, taken directly from decommissioned Minuteman missiles, are mated to the Orion third and fourth stages taken from the Pegasus XL air-launched rocket family. An optional hydrazine-powered fifth stage called HAPS can be used.The Minotaur I launch system is derived from converted Minuteman II ICBMs and is used to launch small satellites for the US Government. An optional hydrazine-powered fifth stage called HAPS can be used.