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
OSCNone
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:
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 OrbitFalcon 9
Starlink Group 10-28
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Soyuz 2.1a
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Shiyan 28 B-01
Launch Complex 3 (LC-3/LA-1) - Xichang Satellite Launch Center, People's Republic of ChinaSatellite officially named for "space environment detection" purposes, exact details unknown.
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Starlink Group 10-25
Space Launch Complex 40 - Cape Canaveral SFS, FL, USAA batch of 27 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
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MTG-S1
Launch Complex 39A - Kennedy Space Center, FL, USASecond of EUMETSAT's third generation of weather satellite.
