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| Eutelsat
2 - Specs |
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Technical Specifications
Eutelsat
2 |
| PAYLOAD
CAPABILITIES |
| Types of Services |
Telecommunication |
| Downlink frequencies |
Ku-band |
| CORE BUS
SPECIFICATIONS |
| Prime Contractor |
Aerospatiale |
| Platform |
Spacebus 2000
|
| Launch Mass |
1878
kg (4139 lbm) |
| Design Life |
9
years |
STRUCTURE |
| Dimensions (H x W x L) |
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| Construction |
|
POWER SYSTEM |
| Payload Power
(EOL) |
3.000
kw |
| Solar Arrays |
2
silicon panels |
| Batteries |
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ATTITUDE CONTROL SYSTEM |
| Stabilization |
3-axis
controlled |
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