Minotaur-C 3210

Active

Orbital 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 America
Vandenberg SFB, CA, USA
May 20, 2004, 5:47 p.m.
Status: Launch Successful
Mission:

ROCSAT 2 (Republic of China Satellite 2) is the second high-resolution Earth observation satellite for the Taiwanese National Space Program Office (NSPO) whose mission is regional remote sensing – to collect data to be used for natural disaster evaluation, agricultural applications, urban planning strategy, environmental monitoring, and ocean surveillance. In addition, the satellite's payload will include an auroral observation instrument.

Medium Earth Orbit
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