적층된 외피를 갖는 샌드위치로 구성된 위성체 안테나 시스템의 모드 해석과 파손안전성 판별 Modal Analysis and Failure Safety Estimation for the Satellite Antenna System Composed of Sandwich Structure with Laminated Face Sheet

Satellite system experiences severe mechanical loads during the launch period. Therefore, positive margin of safety of the satellite system must be demonstrated for every possible mechanical loading condition during the launch period. This paper presents modal and stress analysis result due to quasi-static loads for the satellite antenna system. The failure tendency for the sandwich construction of the satellite antenna system has been studied with various lamination angles of unidirectional prepreg.
Publisher
한국복합재료학회
Issue Date
2001-05
Language
KOR
Citation

한국복합재료학회 춘계학술대회, pp.228 - 233

metadata.dc.identifier.alternativecitation
Proceedings of the 2001 KSCM Spring Conference, pp.228-233
URI
http://hdl.handle.net/10203/8084
Appears in Collection
AE-Conference Papers(학술회의논문)ME-Conference Papers(학술회의논문)AE-Conference Papers(학술회의논문)AE-Conference Papers(학술회의논문)
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