Development of origami-/ kirigami- based strategies for lightweight, stiff and strong structures
The purpose of this project is to develop a deployment system that unfold from a stowed configuration to a large, deployed array configuration. This study is prompted by the need for lightweight and compact folded solar arrays for use in space. In order for solar arrays to be launched in their stowe...
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2023
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sg-ntu-dr.10356-1684162023-06-17T16:50:28Z Development of origami-/ kirigami- based strategies for lightweight, stiff and strong structures Wong, Terry Chiew Hoe Lai Changquan School of Mechanical and Aerospace Engineering cqlai@ntu.edu.sg Engineering::Mechanical engineering The purpose of this project is to develop a deployment system that unfold from a stowed configuration to a large, deployed array configuration. This study is prompted by the need for lightweight and compact folded solar arrays for use in space. In order for solar arrays to be launched in their stowed configuration and then deployed in space with a much larger surface area, the systems require a large ratio of stowed-to-deployed diameter. The objective of the study is to study into different origami folds to further develop folds to increase the packed-to-deployed ratio. Bachelor of Engineering (Mechanical Engineering) 2023-06-12T08:07:28Z 2023-06-12T08:07:28Z 2023 Final Year Project (FYP) Wong, T. C. H. (2023). Development of origami-/ kirigami- based strategies for lightweight, stiff and strong structures. Final Year Project (FYP), Nanyang Technological University, Singapore. https://hdl.handle.net/10356/168416 https://hdl.handle.net/10356/168416 en B109 application/pdf Nanyang Technological University |
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Engineering::Mechanical engineering Wong, Terry Chiew Hoe Development of origami-/ kirigami- based strategies for lightweight, stiff and strong structures |
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The purpose of this project is to develop a deployment system that unfold from a stowed configuration to a large, deployed array configuration. This study is prompted by the need for lightweight and compact folded solar arrays for use in space. In order for solar arrays to be launched in their stowed configuration and then deployed in space with a much larger surface area, the systems require a large ratio of stowed-to-deployed diameter. The objective of the study is to study into different origami folds to further develop folds to increase the packed-to-deployed ratio. |
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Lai Changquan |
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Lai Changquan Wong, Terry Chiew Hoe |
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Final Year Project |
author |
Wong, Terry Chiew Hoe |
author_sort |
Wong, Terry Chiew Hoe |
title |
Development of origami-/ kirigami- based strategies for lightweight, stiff and strong structures |
title_short |
Development of origami-/ kirigami- based strategies for lightweight, stiff and strong structures |
title_full |
Development of origami-/ kirigami- based strategies for lightweight, stiff and strong structures |
title_fullStr |
Development of origami-/ kirigami- based strategies for lightweight, stiff and strong structures |
title_full_unstemmed |
Development of origami-/ kirigami- based strategies for lightweight, stiff and strong structures |
title_sort |
development of origami-/ kirigami- based strategies for lightweight, stiff and strong structures |
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Nanyang Technological University |
publishDate |
2023 |
url |
https://hdl.handle.net/10356/168416 |
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1772828610462220288 |