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| Eutelsat
1 (ECS) - Specs |
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Technical Specifications
Eutelsat
1 (ECS) |
| PAYLOAD
CAPABILITIES |
| Types of Services |
Telecommunication |
| Downlink frequencies |
Ku-band |
| CORE BUS
SPECIFICATIONS |
| Prime Contractor |
Satcom
International (Matra Marconi Space) |
| Platform |
-
|
| Launch Mass |
1185
kg (2612 lbm) |
| Design Life |
9
years |
STRUCTURE |
| Dimensions (H x W x L) |
|
| Construction |
|
POWER SYSTEM |
| Payload Power
(EOL) |
0.900
kw |
| Solar Arrays |
2
silicon panels |
| Batteries |
2
- NiCd, 24 Ahr |
ATTITUDE CONTROL SYSTEM |
| Stabilization |
3-axis
controlled |
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