PK-Minotaur |
Orbital Sciences
Corporation
Orbital Sciences Corporation
announced that it has been awarded a major contract by the
U.S. Air Force to provide space launch and missile defense target vehicles using
deactivated Peacekeeper ICBM assets under the Orbital/Suborbital Program-2 (OSP-2).
Orbital will combine Peacekeeper rocket motors with commercial launch vehicle technology
derived from its Pegasus and Taurus rockets to develop and operate low-cost vehicles
to launch U.S. government-funded satellites into low-Earth orbit. Capable of boosting
payloads more than 1.75 tons into orbit.
Under the Minuteman portion of the contract, Orbital will continue to provide target
and Minotaur space launch services.
The vehicle consists of three Peacekeeper solid rocket stages, a commercial Orion-38
fourth stage motor and subsystems derived from our established space launch boosters.
Under a 10-year contract with the U.S. Air Force Space and Missile Systems Center,
Orbital will develop and operate the low-cost Minotaur-IV vehicle to launch U.S.
government-funded satellites into low-Earth orbit.
The Minotaur-IV
incorporates a standard 92-inch fairing from our Taurus booster and supports dedicated
or shared launch missions. Capable of boosting payloads more than 1,750 kg into
LEO or 998 kg into SSO.
Minotaur-V
is a 5-stage evolutionary version of the Minotaur-IV to launch small spacecraft
into high energy trajectories, including geosynchronous transfer orbits and translunar
missions. The first three stages of the Minotaur-V are the unmodified Peacekeeper
solid rocket motors. The forth and fifth stages are commercial motors. The stage
four motor is nominally a Star-48BV configuration. the fifth stage can be either
attitude controlled or spinning. The attitude controlled version nominally uses
the same Orion-38 motor that has been extensively flight demonstrated on multiple
Orbital launch vehicles. For a spinning configuration, a Star-37FMV is used to provide
maximum performance. The Minotaur avionics, structures, and fairing are common with
the Minotaur-IV SLV. Capable of boosting payloads than 553 to 710 kg
into GTO.
Minotaur-VI
is a Minotaur-IV+ stretched by a second SR-118 motor
on the first stage.
Castor-120XL
This variant of the Castor-120 predecessor is used as a first or second stage in
commercial launch vehicles and provides improved performance over the baseline configuration.
A version of this motor was static tested for the U.S. Air Force as part of the
Large Class Stage development program, however the motor is being updated to tailor
burn rates and improve performance, as well as utilize common materials & processes
to improve cost control for launch vehicle providers.
In addition to Athena family, Castor-120XL is in preparation for Minotaur-C (ex-Taurus
family) and Minotaur-I
(commercial version) which are in the process of being merged into one sub-family
under Minotaur-I.