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| Eutelsat
Hot Bird - Specs |
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Technical Specifications
Eutelsat
Hot Bird |
| PAYLOAD
CAPABILITIES |
| Types of Services |
Telecommunication |
| Downlink frequencies |
Ku-band |
| CORE BUS
SPECIFICATIONS |
| Prime Contractor |
Matra
Marconi Space |
| Platform |
Euorstar 2000+
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| Launch Mass |
2900
kg (6392 lbm) |
| Design Life |
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STRUCTURE |
| Dimensions (H x W x L) |
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| Construction |
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POWER SYSTEM |
| Payload Power
(EOL) |
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| Solar Arrays |
2
silicon panels |
| Batteries |
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ATTITUDE CONTROL SYSTEM |
| Stabilization |
3-axis
controlled |
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