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ORBITAL SCIENCES CORPORATION

Minotaur I

12FLIGHTS
100%SUCCESS
12STREAK
Jan 2000FIRST FLIGHT
NOREUSABLE
HEIGHT19.21 m
DIAMETER1.67 m
LAUNCH MASS36 kg
LIFTOFF THRUST935 kN
STAGES5

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.

580 kg
TO LEO
1,279 lbs
935
KILONEWTONS
210,196
POUNDS-FORCE
~1,254
HORSEPOWER
Height19.21 m (63 ft)
Diameter1.67 m (5.5 ft)
Launch Mass36 kg (79 lbs)
Stages5