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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Bibliographic Details
Main Author: Shivakumar, Ranjana
Other Authors: Teo Hang Tong Edwin
Format: Thesis-Doctor of Philosophy
Language:English
Published: Nanyang Technological University 2020
Subjects:
Online Access:https://hdl.handle.net/10356/143891
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Institution: Nanyang Technological University
Language: English

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