Self-Deployable, Self-Stiffening, and Retractable Origami-Based Arrays for Spacecraft

Author:

Pehrson Nathan A.1,Smith Sam P.1,Ames Daniel C.1,Magleby Spencer P.1,Arya Manan2

Affiliation:

1. Brigham Young University

2. Jet Propulsion Laboratory, California Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Two-Dimensional Array Deployment of Identical Rectangular Panels;AIAA SCITECH 2024 Forum;2024-01-04

2. Design of Membrane Based Unit Cell of Large Reflectarray Antenna for SAR System;2022 IEEE Microwaves, Antennas, and Propagation Conference (MAPCON);2022-12-12

3. Deployment Dynamics Analysis of an Origami-Folded Spacecraft Structure with Elastic Hinges;Journal of Spacecraft and Rockets;2021-09-16

4. Forward dynamics analysis of origami-folded deployable spacecraft structures;Acta Astronautica;2021-09

5. Deployment Experiments of Conceptual Model for Two-Dimensional Self-Deployable Space Structures with Convex-Panels;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2021

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