Minotaur I
OSC
Details
Height
19.21 m
Diameter
1.67 m
GTO
Unknown
LEO
580 kg
Thrust at Liftoff
935 kN
Apogee
Unknown
Launch Cost
Unknown
Maiden Flight
January 27, 2000
Description
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.