Effects of Low-Earth Orbit Space Environment on Structural Mechanics of a Deployable Membrane Space Antenna-Reference-Cited by-同舟云学术

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Effects of Low-Earth Orbit Space Environment on Structural Mechanics of a Deployable Membrane Space Antenna

Published:2007-04-23 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Heald Johanne¹,Jiang Xin Xiang¹

Affiliation:

1. Canadian Space Agency

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-2181

Reference23 articles.

1. Sunshield technology and flight experiment for the Next Generation Space Telescope

2. An algorithm for finite element analysis of partly wrinkled membranes

3. Static and dynamic analysis of partially wrinkled membrane structures

4. New Numerical Method for Two-Dimensional Partially Wrinkled Membranes

Cited by 2 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. A Review on the Development of Spaceborne Membrane Antennas;Space: Science & Technology;2022-01

2. Long-Term Structural Variation of Deployable Membrane Space Antennae;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07

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