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MM-Minotaur - I |
Orbital Sciences
Corporation
The Minotaur - I is a small ground-launched, solid-propellant, and inertally guidespace
launch vehicle composed of components from the Minuteman II ICBM and Pegasus XL
space launch vehicle. It is being developed as part of the US Air Force Orbital/Suborbital
Program (OSP). Prime contractor is Orbital Sciences
Corporation.
The major elements of the vehicle are the M-55A1 motor and SR-19-AJ-1 motor (Minuteman
II/III), Orion 50XL and Orion 38 (Pegasus). The Minotaur first stage utilizes the
existing Minuteman II and III thrust-vector control (TVC) system, which uses four
nozzles to achieve three-axis control. Control during the second stage SR-19 motor
burn is provided by LITVC with warm gas for roll control.
The Minotaur launch vehicle will be capable of placing a 0.336 tons payload into
a 740 km circular, sun-synchronous orbit or a 0.639 tons payload into a 185
km circular orbit. The available payload envelope using the baseline Pegasus fairing
is 1.17 m in diameter for the first 1.22 m above the payload interface plane tapering
to 0.76 m in diameter at the maximum length of 2.24 m.
In addition to the Minotaur I space booster, Orbital's Minotaur product line also includes
