Surface Design Method Incorporating Compression Members for Cable-Mesh Reflectors
The tension truss antenna structure is an effective architecture for large and high-precision parabolic reflectors. Here a parabolic surface is approximated by planar triangular facets formed using cables. However, as the surface area increases or the required accuracy increases, the stiffness of th...
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Veröffentlicht in: | Journal of spacecraft and rockets 2018-01, Vol.55 (1), p.214-222 |
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creator | Miyasaka, Akihiro Takano, Yuichiro Yasui, Noriyasu Nakagawa, Takumi |
description | The tension truss antenna structure is an effective architecture for large and high-precision parabolic reflectors. Here a parabolic surface is approximated by planar triangular facets formed using cables. However, as the surface area increases or the required accuracy increases, the stiffness of the support structure must also increase to prevent its deformation under the increasing strain energy in the cables. This paper proposes a new conceptual cable network for forming parabolic surfaces with low strain energy. Instead of cables, compression members are installed at the rim of the surface so that the strain energy of the cable network is reduced. In this concept, a weight reduction of approximately 25% is possible for the support structure. This design is compared with a conventional cable network, and it is shown that the proposed design is useful in constructing higher-accuracy surface antennas and larger antenna reflectors with lower weight. |
doi_str_mv | 10.2514/1.A33875 |
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Here a parabolic surface is approximated by planar triangular facets formed using cables. However, as the surface area increases or the required accuracy increases, the stiffness of the support structure must also increase to prevent its deformation under the increasing strain energy in the cables. This paper proposes a new conceptual cable network for forming parabolic surfaces with low strain energy. Instead of cables, compression members are installed at the rim of the surface so that the strain energy of the cable network is reduced. In this concept, a weight reduction of approximately 25% is possible for the support structure. This design is compared with a conventional cable network, and it is shown that the proposed design is useful in constructing higher-accuracy surface antennas and larger antenna reflectors with lower weight.</description><identifier>ISSN: 0022-4650</identifier><identifier>EISSN: 1533-6794</identifier><identifier>DOI: 10.2514/1.A33875</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Antennas ; Cables ; Deformation ; Parabolic reflectors ; Reflectors ; Stiffness ; Weight reduction</subject><ispartof>Journal of spacecraft and rockets, 2018-01, Vol.55 (1), p.214-222</ispartof><rights>Copyright © 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at ; employ the ISSN (print) or (online) to initiate your request. See also AIAA Rights and Permissions .</rights><rights>Copyright © 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0022-4650 (print) or 1533-6794 (online) to initiate your request. 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This design is compared with a conventional cable network, and it is shown that the proposed design is useful in constructing higher-accuracy surface antennas and larger antenna reflectors with lower weight.</description><subject>Antennas</subject><subject>Cables</subject><subject>Deformation</subject><subject>Parabolic reflectors</subject><subject>Reflectors</subject><subject>Stiffness</subject><subject>Weight reduction</subject><issn>0022-4650</issn><issn>1533-6794</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2018</creationdate><recordtype>article</recordtype><recordid>eNp90EtLw0AUBeBBFKxV8CcERHCTem9mJsksS3wVWsTXOkySO21Kmokz6cJ_b0pciAtXZ_NxDhzGLhFmkURxi7M552kij9gEJedhnChxzCYAURSKWMIpO_N-C4BxGqsJe3nbO6NLCu7I1-s2WFG_sVWwaEvrOut0X7frILO7zpH3tT2AXUHOB8a6INNFQ-GK_CZ4JdNQ2Vvnz9mJ0Y2ni5-cso-H-_fsKVw-Py6y-TLUHHkfRkmqKqU4KF2pykAhJSKVAJJDjKXQCYJB4ggVVUWKJlYKCkUkIEnTVPMpuxp7O2c_9-T7fGv3rh0m80gokaCSifpP4bAuhjYRDepmVKWz3jsyeefqnXZfOUJ-uDXHfLx1oNcj1bXWv8r-um8XVnM9</recordid><startdate>201801</startdate><enddate>201801</enddate><creator>Miyasaka, Akihiro</creator><creator>Takano, Yuichiro</creator><creator>Yasui, Noriyasu</creator><creator>Nakagawa, Takumi</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>201801</creationdate><title>Surface Design Method Incorporating Compression Members for Cable-Mesh Reflectors</title><author>Miyasaka, Akihiro ; Takano, Yuichiro ; Yasui, Noriyasu ; Nakagawa, Takumi</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a313t-2789d99309ad9df0b5511ec0053061c4a710f1e310dedb81f6990b9ee407888a3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2018</creationdate><topic>Antennas</topic><topic>Cables</topic><topic>Deformation</topic><topic>Parabolic reflectors</topic><topic>Reflectors</topic><topic>Stiffness</topic><topic>Weight reduction</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Miyasaka, Akihiro</creatorcontrib><creatorcontrib>Takano, Yuichiro</creatorcontrib><creatorcontrib>Yasui, Noriyasu</creatorcontrib><creatorcontrib>Nakagawa, Takumi</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>Miyasaka, Akihiro</au><au>Takano, Yuichiro</au><au>Yasui, Noriyasu</au><au>Nakagawa, Takumi</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Surface Design Method Incorporating Compression Members for Cable-Mesh Reflectors</atitle><jtitle>Journal of spacecraft and rockets</jtitle><date>2018-01</date><risdate>2018</risdate><volume>55</volume><issue>1</issue><spage>214</spage><epage>222</epage><pages>214-222</pages><issn>0022-4650</issn><eissn>1533-6794</eissn><abstract>The tension truss antenna structure is an effective architecture for large and high-precision parabolic reflectors. 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subjects | Antennas Cables Deformation Parabolic reflectors Reflectors Stiffness Weight reduction |
title | Surface Design Method Incorporating Compression Members for Cable-Mesh Reflectors |
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