Minotaur I

Overview
/01The 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.
Manufacturer
Variant
Alias
Maiden Flight
Technical Specifications
/02Length
Diameter
Launch Mass
Liftoff Thrust
LEO Capacity
GTO Capacity
Launch Record
/03Total Launches
Successful
Failed
Success Rate
Attempted Landings
Successful Landings
Failed Landings
Consecutive Successes