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ETS-VIII |
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| Client |
NASDA (now JAXA) |
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| Launch date |
December 18, 2006 |
| Launch vehicle |
H-IIA |
| Launch site |
Tanegashima Space Center |
| Orbit |
Geostationary orbit |
| Weight |
2,800 kg (at launch) |
| Electrical power |
7,500 W |
| Design life |
10 years (satellite bus)
3 years (mission craft) |
| Responsibilities |
Prime contractor |
| Outline |
| The ETS-VIII's missions are to develop technologies, and test and verify them in space. The targeted technologies include mobile-satellite communications, mobile-satellite digital multimedia, and basic technologies for building satellite positioning systems, through large-scale geosynchronous satellite bus technologies for 3-ton class satellites -- the world's largest class in the early 2000s. The ETS-VIII also targets such large-scale deployable antenna technologies as 13 meter-class deployable antennas, and high-accuracy time standard systems and other positioning equipment. |
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