Structure Design for TUUSAT-1A Microsatellite | |
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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 | en |
ISSN | 1991-8747 |
期刊性質 | 國外 |
收錄於 | EI |
產學合作 | |
通訊作者 | |
審稿制度 | |
國別 | GRC |
公開徵稿 | |
出版型式 | 紙本 |
相關連結 |
機構典藏連結 ( http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/65387 ) |