Deployment Dynamics Analysis of an Origami-Folded Spacecraft Structure with Elastic Hinges
Author:
Affiliation:
1. University of Colorado Boulder, Boulder, Colorado 80303-0429
Funder
NASA Space Technology Research Fellowship
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A34938
Reference25 articles.
1. MegaFlex - The Scaling Potential of UltraFlex Technology
2. Fundamental Design of Tensioned Precision Deployable Space Structures Applied to an X-Band Phased Array
3. Folding Approaches for Tensioned Precision Planar Shell Structures
4. Novel Folding Methods for Deterministic Deployment of Common Space Structures
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