3D-C/shape memory polymer composite for space deployable applications
Large components such as solar panels, solar sails and antenna in the satellite are generally designed as deployable structures, that are stowed during launch and deployed in orbit using electromechanical deployment systems. The structural integrity, reliability, weight and stowage volume of the dep...
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Main Author: | Shivakumar, Ranjana |
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Other Authors: | Teo Hang Tong Edwin |
Format: | Thesis-Doctor of Philosophy |
Language: | English |
Published: |
Nanyang Technological University
2020
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Subjects: | |
Online Access: | https://hdl.handle.net/10356/143891 |
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Institution: | Nanyang Technological University |
Language: | English |
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