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The
primary objective of the ROCSAT 2 (ROC Satellite No. 2) satellite
mission is to observe and monitor the terrestrial and marine
environment and natural resources throughout Taiwan, its remote
islands and surrounding ocean for civil applications. In addition,
the ROCSAT 2 satellite also carries a 'Sprites Imager' scientific
instrument to study the electrodynamical coupling between
thunderclouds and the upper atmosphere by taking images of
lightening discharges.
The
700 kg (1543 lbm) satellite will be placed in a 890 km (480 nmi)
sun-synchronous orbit with a 98.99 degree inclination. It is
planned for a 5 year mission.
The
US$75 million (2.37 billion Taiwan dollars) ROCSAT 2 program was
approved in Oct 1997. NPSO has signed a contract with France's
Matra Marconi Space on November 29, 1999, to build the ROCSAT 2
satellite, after canceling a contract with a German consortium
because of pressure from mainland China. Matra Marconi Space is
responsible for the satellite's payload and bus, with the rest of
the project to be completed by six Taiwanese companies, including
Acer, Tatung, Shihlin Electric & Engineering and Tay Yung
Engineering Co. to supply components such as flight software,
S-band antennae and other computer equipment for the project.
ROCSAT 2 will be the first application for Matra Marconi’s
standard small satellite bus, Leostar. Matra Marconi Space was the
losing bidder in the original round, and has been able to secure
French government approval for an export sale.
DaimlerChrysler
Aerospace’s Dornier Satelliten unit had won a bid to build
ROCSAT 2 for Taiwan's National Space Program February 8, 1999.
However, the company was forced to back out of the contract on
November 5, 1999, when the German government refused to grant an
export permit for satellite-related technology to Taiwan. The
US$600,000 deposit was returned to the Taiwanese government. Matra
Marconi Space and Dornier Satelliten are now both of Astrium.
ROCSAT
2
Republic
of
China
Satellite
No. 2
|
|
SATELLITE
|
| Int'l Designation |
|
Scheduled
|
| Owner / Sponsor |
NPSO
(Taiwan) / National
Space Program Office
|
| Mission |
Observation
|
| Satellite bus |
Astrium
(Matra Marconi Space)
|
LEOSTAR
|
| Launch Mass |
700
kg (1543 lbm)
|
| Dimensions, stowed |
|
| Mission Orbit |
SSO
/ 890 km (480 nmi)
|
98.99°
|
| Design Life |
5
years
|
| Power (EOL) |
|
|
LAUNCH
|
| Launch Vehicle
Model |
Taurus |
| Date / Time (UTC) |
2003
|
|
|
FINANCIAL
|
| Satellite cost |
US$75
million (2.37 billion Taiwan dollars)
|
| Web Links |
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