Design and Testing of Self-Deploying Membrane Optic Support Structure Using Rollable Composite Tape Springs

Author:

Footdale Joseph N.1,Murphey Thomas W.2,Peterson Michael E.3

Affiliation:

1. LoadPath

2. Air Force Research Laboratory

3. University of New Mexico

Publisher

American Institute of Aeronautics and Astronautics

Cited by 7 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. Analysis of the designs of membrane transformable antennas for spacecraft;Spacecrafts & Technologies;2022-09-26

2. Experiments and Simulations of the Deployment of a Bistable Composite Boom;Journal of Spacecraft and Rockets;2018-03

3. Deployment of Bistable Self-Deployable Tape Spring Booms Using a Gravity Offloading System;Journal of Aerospace Engineering;2017-07

4. Flight Qualification Testing of a Meter-class CubeSat Deployable Boom;4th AIAA Spacecraft Structures Conference;2017-01-05

5. Control-oriented modeling and deployment of tensegrity-membrane systems;International Journal of Robust and Nonlinear Control;2016-12-27

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