Vehicle / SINCE 2000

Minotaur I

ABOUT

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.

SPECIFICATIONS 9
Length 19.21 m
Diameter 1.67 m
Launch Mass T 36
Leo Capacity 580 kg
Thrust 935 kN
Reusable No
Total Launches 12
Successful Launches 12
Maiden Flight 2000-01-27