Minotaur-C 1110
ActiveOrbital Sciences Corporation (OSC)
March 12, 2000
Description
American all-solid orbital launch vehicle based on a Pegasus and Peacekeeper rocket.It has been designed as a quick reaction launch vehicle, which can be launched from minimaly prepared places in a matter of a few days.
Specifications
-
Stages
4 -
Length
27.9 m -
Diameter
2.35 m -
Fairing Diameter
2.35 m -
Launch Mass
73.0 T -
Thrust
1320.0 kN
Family
-
Name
Minotaur-C 1110 -
Family
― -
Variant
1110 -
Alias
― -
Full Name
Minotaur-C 1110
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
1320.0 kg -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
Orbital Sciences Corporation
Commercial
None
OSCNone
Taurus 1110 | MTI
Orbital Sciences Corporation | United States of AmericaVandenberg SFB, CA, USA
March 12, 2000, 9:29 a.m.
Status: Launch Successful
Mission:
The primary objective of MTI (Multispectral Thermal Imager) was to demonstrate advanced multispectral and thermal imaging, image processing, and associated technologies that could be used in future systems for detecting and characterizing facilities producing weapons of mass destruction using radiometrically accurate, high spatial resolution, multispectral imaging.
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