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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...
| Autores principales: | , , , , , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
MDPI
2022
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| Materias: | |
| 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 |