Effect of Boundary Support and Reflector Dimensions on Inflatable Parabolic Antenna Performance
For parabolic antennas with sufficient surface accuracy, more power can be radiated with a larger aperture size. This paper explores the performance of antennas of various size and reflector depth. The particular focus is on a large inflatable elastic antenna reflector that is supported about its pe...
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Veröffentlicht in: | Journal of spacecraft and rockets 2012-09, Vol.49 (5), p.905-914 |
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creator | Coleman, Michael J Baginski, Frank Romanofsky, Robert R |
description | For parabolic antennas with sufficient surface accuracy, more power can be radiated with a larger aperture size. This paper explores the performance of antennas of various size and reflector depth. The particular focus is on a large inflatable elastic antenna reflector that is supported about its perimeter by a set of elastic tendons and is subjected to a constant hydrostatic pressure. The surface accuracy of the antenna is measured by an rms calculation, whereas the reflector phase error component of the efficiency is determined by computing the power density at boresight. In the analysis, the calculation of antenna efficiency is not based on the Ruze Equation. Hence, no assumption regarding the distribution of the reflector surface distortions is presumed. The reflector surface is modeled as an isotropic elastic membrane using a linear stress-strain constitutive relation. Three types of antenna reflector construction are considered: one molded to an ideal parabolic form and two different flat panel design patterns. The flat panel surfaces are constructed by seaming together panels in a manner that the desired parabolic shape is approximately attained after pressurization. Numerical solutions of the model problem are calculated under a variety of conditions to estimate the accuracy and efficiency of these antenna systems. In the case of the flat panel constructions, several different cutting patterns are analyzed to determine an optimal cutting strategy. |
doi_str_mv | 10.2514/1.A32021 |
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This paper explores the performance of antennas of various size and reflector depth. The particular focus is on a large inflatable elastic antenna reflector that is supported about its perimeter by a set of elastic tendons and is subjected to a constant hydrostatic pressure. The surface accuracy of the antenna is measured by an rms calculation, whereas the reflector phase error component of the efficiency is determined by computing the power density at boresight. In the analysis, the calculation of antenna efficiency is not based on the Ruze Equation. Hence, no assumption regarding the distribution of the reflector surface distortions is presumed. The reflector surface is modeled as an isotropic elastic membrane using a linear stress-strain constitutive relation. Three types of antenna reflector construction are considered: one molded to an ideal parabolic form and two different flat panel design patterns. The flat panel surfaces are constructed by seaming together panels in a manner that the desired parabolic shape is approximately attained after pressurization. Numerical solutions of the model problem are calculated under a variety of conditions to estimate the accuracy and efficiency of these antenna systems. 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The flat panel surfaces are constructed by seaming together panels in a manner that the desired parabolic shape is approximately attained after pressurization. Numerical solutions of the model problem are calculated under a variety of conditions to estimate the accuracy and efficiency of these antenna systems. In the case of the flat panel constructions, several different cutting patterns are analyzed to determine an optimal cutting strategy.</description><subject>Accuracy</subject><subject>Antennas</subject><subject>Computational efficiency</subject><subject>Computing time</subject><subject>Construction</subject><subject>Flat panels</subject><subject>Mathematical models</subject><subject>Parabolic antennas</subject><subject>Reflectors</subject><issn>0022-4650</issn><issn>1533-6794</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2012</creationdate><recordtype>article</recordtype><recordid>eNqF0UtLxDAQB_AgCq4P8CMERPBSzeTV5ri-BUHxcQ7ZdAKVbrIm7cFvb2UFxYOe5jA__sPMEHIA7IQrkKdwMheccdggM1BCVLo2cpPMGOO8klqxbbJTyitjoBttZsRehoB-oCnQszTG1uV3-jSuVikP1MWWPmLop37K9KJbYixdioWmSG9j6N3gFj3SB5fdIvWdp_M4YIyOPmAOKS9d9LhHtoLrC-5_1V3ycnX5fH5T3d1f357P7yonQQyVRG20WnjOtDTK-QbboKRvpDABOQLzhuGiVd7UjUTeOsm4DAiBtQ0IL8UuOV7nrnJ6G7EMdtkVj33vIqaxWNA1TOsrUf9PuZ6wqutmooe_6Gsac5wWsRw01EJr-FOB0Mpw2TDzPdbnVErGYFe5W073tsDs5-ss2PXrJnq0pq5z7kfYb_cBiVKUag</recordid><startdate>20120901</startdate><enddate>20120901</enddate><creator>Coleman, Michael J</creator><creator>Baginski, Frank</creator><creator>Romanofsky, Robert R</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20120901</creationdate><title>Effect of Boundary Support and Reflector Dimensions on Inflatable Parabolic Antenna Performance</title><author>Coleman, Michael J ; Baginski, Frank ; Romanofsky, Robert R</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a413t-4e6965bc206495ac8edf54c8439fe2e10c90ebd5c9784e2da4024fe1f0d813c43</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2012</creationdate><topic>Accuracy</topic><topic>Antennas</topic><topic>Computational efficiency</topic><topic>Computing time</topic><topic>Construction</topic><topic>Flat panels</topic><topic>Mathematical models</topic><topic>Parabolic antennas</topic><topic>Reflectors</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Coleman, Michael J</creatorcontrib><creatorcontrib>Baginski, Frank</creatorcontrib><creatorcontrib>Romanofsky, Robert R</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Journal of spacecraft and rockets</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Coleman, Michael J</au><au>Baginski, Frank</au><au>Romanofsky, Robert R</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Effect of Boundary Support and Reflector Dimensions on Inflatable Parabolic Antenna Performance</atitle><jtitle>Journal of spacecraft and rockets</jtitle><date>2012-09-01</date><risdate>2012</risdate><volume>49</volume><issue>5</issue><spage>905</spage><epage>914</epage><pages>905-914</pages><issn>0022-4650</issn><eissn>1533-6794</eissn><abstract>For parabolic antennas with sufficient surface accuracy, more power can be radiated with a larger aperture size. 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The flat panel surfaces are constructed by seaming together panels in a manner that the desired parabolic shape is approximately attained after pressurization. Numerical solutions of the model problem are calculated under a variety of conditions to estimate the accuracy and efficiency of these antenna systems. In the case of the flat panel constructions, several different cutting patterns are analyzed to determine an optimal cutting strategy.</abstract><cop>Reston</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.A32021</doi><tpages>10</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Accuracy Antennas Computational efficiency Computing time Construction Flat panels Mathematical models Parabolic antennas Reflectors |
title | Effect of Boundary Support and Reflector Dimensions on Inflatable Parabolic Antenna Performance |
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