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Manuscript template and style guide

  • Aerospace System Engineering Shanghai
  • Shanghai Key Laboratory of Spacecraft Mechanism

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

This paper puts forward a new concept of flexible solar array, which includes lenticular tube, polyimide membrane and triple junction solar cells. Parametric study was performed on a flexible solar array design to identify parameters of interest. The FEA software, ABAQUS, was used to perform the structural analysis to simulate the stiffness of solar array. A full-scale solar array including inertia relief and geometric nonlinearity has been presented. The numerical analysis procedures to introduce pre-stress load into flexible panel were presented firstly, and a rectangle panel was evaluated as a typical example. There are many factors which affect the stiffness of flexible solar array, and they interrelate with each other. Therefore, orthogonal method including four factors, such as membrane's tension, membrane's thickness, lenticular tube's sectional radius and lenticular tube's thickness, has been studiedd in the numerical analysis. Through the Range Analysis of the orthogonal experiment, the main factors affecting the stiffness of solar array have been achieved, and the structural parameters have been optimized.

Original languageEnglish
Title of host publication64th International Astronautical Congress 2013, IAC 2013
PublisherInternational Astronautical Federation, IAF
Pages5758-5764
Number of pages7
ISBN (Print)9781629939094
StatePublished - 2013
Externally publishedYes
Event64th International Astronautical Congress 2013, IAC 2013 - Beijing, China
Duration: 23 Sep 201327 Sep 2013

Publication series

NameProceedings of the International Astronautical Congress, IAC
Volume7
ISSN (Print)0074-1795

Conference

Conference64th International Astronautical Congress 2013, IAC 2013
Country/TerritoryChina
CityBeijing
Period23/09/1327/09/13

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