Additive Manufacturing of Lightweight, Optimized, Metallic Components Suitable for Space Flight
A holistic process flow designed and implemented for additive manufacturing of topology-optimized metallic components suitable for use on satellites is described and demonstrated with two components that are part of the Surrey Satellite Technology, Ltd. technology mission. The holistic process flow...
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Veröffentlicht in: | Journal of spacecraft and rockets 2017-09, Vol.54 (5), p.1050-1059 |
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container_title | Journal of spacecraft and rockets |
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creator | Orme, Melissa E Gschweitl, Michael Ferrari, Michael Vernon, Russell Madera, Ivan J Yancey, Robert Mouriaux, Franck |
description | A holistic process flow designed and implemented for additive manufacturing of topology-optimized metallic components suitable for use on satellites is described and demonstrated with two components that are part of the Surrey Satellite Technology, Ltd. technology mission. The holistic process flow begins with part selection and includes topology optimization, finite element analysis verification, additive manufacturing, and an aggressive mechanical and material testing campaign. The case studies used in this work include a camera bracket and a satellite panel insert. Both parts were fabricated under the guidelines of the holistic process flow in a total of eight weeks from concept to verification for flight. The process flow includes verification feedback loops in the design stage and the manufacturing stage. The aggressive testing campaign that is the last step in the process flow is included in order to guarantee the mechanical fidelity of the additively manufactured, produced components intended for flight approval and to demonstrate that the project specifications are met. |
doi_str_mv | 10.2514/1.A33749 |
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The holistic process flow begins with part selection and includes topology optimization, finite element analysis verification, additive manufacturing, and an aggressive mechanical and material testing campaign. The case studies used in this work include a camera bracket and a satellite panel insert. Both parts were fabricated under the guidelines of the holistic process flow in a total of eight weeks from concept to verification for flight. The process flow includes verification feedback loops in the design stage and the manufacturing stage. The aggressive testing campaign that is the last step in the process flow is included in order to guarantee the mechanical fidelity of the additively manufactured, produced components intended for flight approval and to demonstrate that the project specifications are met.</description><identifier>ISSN: 0022-4650</identifier><identifier>EISSN: 1533-6794</identifier><identifier>DOI: 10.2514/1.A33749</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Additive manufacturing ; Feedback loops ; Finite element method ; Project specifications ; Satellites ; Space flight ; Topology optimization ; Verification</subject><ispartof>Journal of spacecraft and rockets, 2017-09, Vol.54 (5), p.1050-1059</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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subjects | Additive manufacturing Feedback loops Finite element method Project specifications Satellites Space flight Topology optimization Verification |
title | Additive Manufacturing of Lightweight, Optimized, Metallic Components Suitable for Space Flight |
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