Minotaur-C 2110
ActiveOrbital Sciences Corporation (OSC)
Sept. 21, 2001
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
1380.0 kN
Family
-
Name
Minotaur-C 2110 -
Family
― -
Variant
2110 -
Alias
― -
Full Name
Minotaur-C 2110
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
1380.0 kg -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
Orbital Sciences Corporation
Commercial
None
OSCNone
Taurus 2110 | OrbView-4
Orbital Sciences Corporation | United States of AmericaVandenberg SFB, CA, USA
Sept. 21, 2001, 6:49 p.m.
Status: Launch Failure
Mission:
Orbview 4 was a high resolution commercial Earth imaging satellite imagery. OrbView 4's imaging instrument was to provide one-meter panchromatic imagery and four-meter multispectral imagery. OrbView 4 was lost in an launch failure, when the Taurus-2110 carrier rocket suffered an loss of control, which was recovered, but orbit was not achieved.
Sun-Synchronous OrbitTaurus 2110 | Arirang-1 & ACRIMSat
Orbital Sciences Corporation | United States of AmericaVandenberg SFB, CA, USA
Dec. 21, 1999, 7:13 a.m.
Status: Launch Successful
Mission:
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