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