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When Deployable Spacecraft Antennas Don’t

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dc.contributor.author Cable, Vaughn
dc.date.accessioned 2020-04-21T00:16:33Z
dc.date.available 2020-04-21T00:16:33Z
dc.date.issued 2018-07-08
dc.identifier.citation 2018 IEEE International Symposium on Antennas and Propagation and USNC-URSI Radio Science Meeting, Boston, Massachusetts, July 8-13, 2018 en_US
dc.identifier.clearanceno 18-0285
dc.identifier.uri http://hdl.handle.net/2014/47989
dc.description.abstract The objective of this paper is to explore possibilities for continued use of certain deployable spacecraft antennas when full deployment fails. Four (4) deployables are used as examples, including 1) a reflectarray, 2) a parabolic reflector, 3) a loop, and 4) a set of 4 monopoles. The measure of “continued usability” in each case is relative antenna gain as a function of partial deployment. Note, types (and levels) of partial deployment presented here are strictly hypothetical. Also, discussions of actual deployment mechanisms are considered outside the scope of this paper. en_US
dc.description.sponsorship NASA/JPL en_US
dc.language.iso en_US en_US
dc.publisher Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2018 en_US
dc.title When Deployable Spacecraft Antennas Don’t en_US
dc.type Preprint en_US


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