航空宇宙技術
Online ISSN : 1884-0477
ISSN-L : 1884-0477
次期高性能静止衛星構体の開発
高野 敦高野 千尋早田 康三石島 義之宇都宮 真清水 隆三
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ジャーナル フリー

2011 年 10 巻 p. 75-82

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The development of bus-structure for the further GEO satellite is described. The target of the further GEO satellite is to be the satellite with 8 kW solar generation, 3650 kg launch weight, and sufficiently global competitiveness on the next decade. The target weight of the bus-structure is lower than 215 kg (lower than 5.9 % of launch weight). The design and mechanical tests of the bus structure have been successfully completed.

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© 2011 The Japan Society for Aeronautical and Space Sciences
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