關鍵字查詢 | 類別:期刊論文 | | 關鍵字:Structure Design for TUUSAT-1A Microsatellite

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1 98/1 機電系 洪祖昌 教授 期刊論文 發佈 Structure Design for TUUSAT-1A Microsatellite , [98-1] :Structure Design for TUUSAT-1A Microsatellite期刊論文Structure Design for TUUSAT-1A MicrosatelliteLin, Chin-feng; Hong, Zuu-chang; Chern, Jeng-shing; Lin, Chien-ming; Chang, Bo-jyun; Fong, Chen-joe; Lin, Huan-jung淡江大學機械與機電工程學系structure; microsatellite; reliability; safety; effectiveness; stable operationZographou: World Scientific and Engineering Academy and Society (W S E A S)WSEAS Transactions On Applied And Theoretical Mechanics 5(1), pp.45-58One of the main advantage of microsatellites is their small size. The reliability, safety, and effectiveness of the satellite structure play an important role in the normal operation of the satellite. The satellite structure should be designed that it supports all subsystems, and payloads. The satellite structure should be stable against vibration and environmental factors during the rocket launch, in order to ensure normal operation of the other subsystems and payload. When designing a satellite, we take into account the features of the attitude c
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