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dc.contributor.authorCaparrós, Andrés
dc.contributor.authorBecedas, Jonathan
dc.date.accessioned2021-06-02T10:11:33Z
dc.date.available2021-06-02T10:11:33Z
dc.date.issued2019
dc.identifierONIX_20210602_10.5772/intechopen.78762_407
dc.identifier.urihttps://library.oapen.org/handle/20.500.12657/49293
dc.description.abstractSpace debris has become a major aspect in the last few years. The vast amount of artificial objects orbiting the Earth is increasing. These objects are a threat for active and future missions. Besides, the possibility of uncontrolled re-entry of some of them reaching the surface of the Earth exists. The aim of this work is to provide a view on how to use additive manufacturing technology to design the next generation of satellites in order to reduce the space debris. The components that can be manufactured with additive manufacturing are identified, together with the technologies that are enabled by additive manufacturing to reduce space debris. Finally, the results of these studies and analysis are incorporated into the design of the structure of a small satellite. This study is being part of the H2020 European Project ReDSHIFT (Project ID 687500).
dc.languageEnglish
dc.subject.classificationthema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues::TBC Engineering: generalen_US
dc.subject.otheradditive manufacturing, space debris, satellite structural design, ReDSHIFT H2020 project
dc.subject.otherCubeSat, impacts mitigation
dc.titleChapter Additive Manufacturing Applied to the Design of Small Satellite Structure for Space Debris Reduction
dc.typechapter
oapen.identifier.doi10.5772/intechopen.78762
oapen.relation.isPublishedBy09f6769d-48ed-467d-b150-4cf2680656a1
oapen.relation.isFundedByH2020-PROTEC-2015
oapen.grant.number687500
oapen.grant.acronymReDSHIFT


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