Minotaur-C 3210
ActiveOrbital Sciences Corporation (OSC)
May 20, 2004
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
31.6 m -
Diameter
2.35 m -
Fairing Diameter
2.35 m -
Launch Mass
73.0 T -
Thrust
1380.0 kN
Family
-
Name
Minotaur-C 3210 -
Family
― -
Variant
3210 -
Alias
― -
Full Name
Minotaur-C 3210
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
― -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
Orbital Sciences Corporation
Commercial
None
OSC
Taurus 3210 | Formosat-2
Orbital Sciences Corporation | United States of AmericaVandenberg SFB, CA, USA
May 20, 2004, 5:47 p.m.
Status: Launch Successful
Mission:
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