Umali, James and Wilson, Lee and Pellegrino, Sergio (2017) Vibration Response of Ultralight Coilable Spacecraft Structures. In: 4th AIAA Spacecraft Structures Conference. American Institute of Aeronautics and Astronautics , Reston, VA, Art. No. 2017-1115. ISBN 978-1-62410-455-8. https://resolver.caltech.edu/CaltechAUTHORS:20190820-152401055
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Abstract
Dynamic assessment of ultralight wrapped spacecraft structures subject to the launch vibration environment is difficult, and has been foregone in many space programs in favor of purely experimental test campaigns. We present a numerical methodology to better understand the wrapped state of a structure and the dynamic behavior during launch vibration, enabling higher confidence in its survivability and greater understanding of the dynamic behavior at different scales, which vibration test approaches alone cannot achieve.
Item Type: | Book Section | ||||||
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Additional Information: | © 2017 American Institute of Aeronautics and Astronautics. Published Online: 5 Jan 2017. Financial support from Northrop Grumman Corporation is gratefully acknowledged. | ||||||
Group: | GALCIT, Space Solar Power Project | ||||||
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DOI: | 10.2514/6.2017-1115 | ||||||
Record Number: | CaltechAUTHORS:20190820-152401055 | ||||||
Persistent URL: | https://resolver.caltech.edu/CaltechAUTHORS:20190820-152401055 | ||||||
Official Citation: | Vibration Response of Ultralight Coilable Spacecraft Structures. James A. Umali, Lee L. Wilson, and Sergio Pellegrino. 4th AIAA Spacecraft Structures Conference. January 2017. https://doi.org/10.2514/6.2017-1115 | ||||||
Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. | ||||||
ID Code: | 98049 | ||||||
Collection: | CaltechAUTHORS | ||||||
Deposited By: | Tony Diaz | ||||||
Deposited On: | 20 Aug 2019 22:44 | ||||||
Last Modified: | 16 Nov 2021 17:36 |
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