CubeSat’s Deployable Solar Panel with Viscoelastic Multilayered Stiffener for Launch Vibration Attenuation
Ensuring the structural safety of a deployable solar panel under a severe launch vibration environment is one of the important factors for a successful CubeSat mission. A CubeSat’s deployable solar panel proposed in this study is effective to guarantee the structural safety of solar cells by attenua...
Main Authors: | Shankar Bhattarai, Hongrae Kim, Hyun-Ung Oh |
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Format: | Article |
Language: | English |
Published: |
Hindawi Limited
2020-01-01
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Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2020/8820619 |
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