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SERVIS |
|
| Client |
USEF |
 |
| Launch date |
#1: October 30, 2003
#2: Fiscal 2008 |
| Launch vehicle |
#1: Rocket
#2: TBD |
| Launch site |
#1: Plesetsk Space Center, Russia
#2: TBD |
| Orbit |
#1: Altitude: 1,000 - 1,500 km
Circular orbit, Inclination: 30 deg.
#2: Altitude: 1,000 km or higher
Circular orbit, Inclination: 97 deg. |
| Weight |
#1: Approx. 980 kg
#2: Approx. 980 kg |
| Electrical power |
#1: 1,200 W |
| Design life |
5 years |
| Responsibilities |
Prime contractor |
| Outline |
Space Environmental Reliability Verification Integrated System (SERVIS)
Mission:
Verify civilian parts and equipment in space for low-cost, short-cycle, high-quality (CFB) satellites. The development of SERVIS 1 and 2 will result in a low-cost commercial bus. |
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