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Please use this identifier to cite or link to this item:
http://hdl.handle.net/2014/40204
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| Title: | Preliminary analysis of the 30-m UltraBoom flight test |
| Authors: | Agnes, Gregory S. Abelson, Robert D. Miyake, Robert Lin, John K. H. Welsh, Joe Watson, Judith J. |
| Keywords: | UltraBoom isogrid lightweight booms |
| Issue Date: | 18-Apr-2005 |
| Publisher: | Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2005. |
| Citation: | 46th Structural Dynamics and Materiels Conference, Austin, Texas, April 18-21, 2005. |
| Abstract: | Future NASA missions require long, ultra-lightweight booms to enable solar sails, large sunshields, and other gossamer-type spacecraft structures. The space experiment discussed in this paper will flight validate the non-traditional ultra lightweight rigidizable, inflatable, isogrid structure utilizing graphite shape memory polymer (GR/SMP) called UltraBoomâ„¢. The focus of this paper is the analysis of the 3-m ground test article. The primary objective of the mission is to show that a combination of ground testing and analysis can predict the on-orbit performance of an ultra lightweight boom that is scalable, predictable, and thermomechanically stable |
| URI: | http://hdl.handle.net/2014/40204 |
| Appears in Collections: | JPL TRS 1992+
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