Configuration Design and Dynamic Characteristics Analysis of Spacecraft Membrane Sunshield

To meet the needs of large space telescopes, such as light weight, high folding ratio, and low manufacturing cost, a flexible deployable regular hexagonal membrane sunshield is proposed in this paper. Firstly, the dynamic equation of the membrane plane is established by the micro-element method. The...

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Detalles Bibliográficos
Autores principales: Peng, Tao, Lin, Qiuhong, Li, Bingyan, Dai, Shuwu, Luo, Ani, Cong, Qiang, Liu, Rongqiang
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8839450/
https://www.ncbi.nlm.nih.gov/pubmed/35160598
http://dx.doi.org/10.3390/polym14030609

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8839450/
https://www.ncbi.nlm.nih.gov/pubmed/35160598
http://dx.doi.org/10.3390/polym14030609

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