教師資料查詢 | 類別: 期刊論文 | 教師: 洪祖昌 Hong Zuu-chang (瀏覽個人網頁)

標題:Structure Design for TUUSAT-1A Microsatellite
學年98
學期1
出版(發表)日期2010/01/01
作品名稱Structure Design for TUUSAT-1A Microsatellite
作品名稱(其他語言)
著者Lin, Chin-feng; Hong, Zuu-chang; Chern, Jeng-shing; Lin, Chien-ming; Chang, Bo-jyun; Fong, Chen-joe; Lin, Huan-jung
單位淡江大學機械與機電工程學系
出版者Zographou: World Scientific and Engineering Academy and Society (W S E A S)
著錄名稱、卷期、頁數WSEAS Transactions On Applied And Theoretical Mechanics 5(1), pp.45-58
摘要One 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 control subsystem, thermal control subsystem, and solar energy subsystem, which are essential for stable operation, as well as the reliability of the structure. In this article, we discuss a structure design for the Taiwan Universities United Satellite NO.1A (TUUSAT-1A) microsatellite. The satellite is a cube with an edge of 28 cm. The surface of the satellite is covered by six aluminum plates, each of which has a solar chip attached to it. The satellite mainly comprises four layers-each layer is an aluminum plates that form a single aluminum alloy block.
關鍵字structure; microsatellite; reliability; safety; effectiveness; stable operation
語言英文
ISSN1991-8747
期刊性質國外
收錄於EI
產學合作
通訊作者
審稿制度
國別希臘
公開徵稿
出版型式紙本
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