Efficient Storage and Deployment of Tubular Composite Boom Using Spring Root Hinges
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
2. Sakase Adtech Company, Ltd., Maruoka 910-0363, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference14 articles.
1. Progress in Astronautics and Aeronautics;Murphey T. W.,2006
2. Deployment dynamics of tape springs
3. Folding and deployment of curved tape springs
4. Analysis of tape spring hinges
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1. Root Boundary Conditions for Omega Deployable Booms;AIAA SCITECH 2024 Forum;2024-01-04
2. Folding, stowage, and deployment of composite thin-walled lenticular tubes;Acta Astronautica;2023-12
3. Analysis and tests of non-uniform wrapping process of tape spring;International Journal of Solids and Structures;2023-10
4. TRAC-Spring Guided Hinges;AIAA SCITECH 2022 Forum;2022-01-03
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