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CHIPSat will map the
entire sky to a depth of about 40,000 seconds per resolution
element (resel). Each resel is 5° × 26.7°; approximately 316
resels are required to cover the entire sky. This map should
provide high S/N detections of the strongest emission lines.
SpaceDev is under
contract to design and build the spacecraft, integrate the science
payload, integrate the flight system to the launch vehicle, and
operate the CHIPSat Observatory for one year. CHIPSat is a
three-axis stabilized spacecraft, with a solar-panel array roughly
orthogonal to the field of view of the spectrograph. The mission
will last one year.
CHIPSat
Cosmic
Hot
Interstellar
Plasma
Spectrometer
|
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SPACECRAFT
|
| Int'l Designation |
2003 002B
|
Launched
|
| Owner / Sponsor |
NASA
/ University of California, Berkeley
|
| Mission |
Science
|
| Satellite Bus |
SpaceDev,
Inc
|
|
| Launch Mass |
60
kg (131 lbm)
|
| Mission Orbit |
SSO /
600 km (324 nmi)
|
94°
|
| Design Life |
1
year
|
| Power (EOL) |
|
|
LAUNCH
|
| Launch Vehicle
Model |
Delta
2 7320-10 |
| Launch Date / Time |
13
January 2003
|
00:45
|
| Co-passenger(s) |
ICESat |
|
FINANCIAL
|
| Satellite cost |
US$12
million
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| Web Links |
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