Ground-based laser effect on space debris maneuvering

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Autor(es): dc.contributorUniversidade Estadual Paulista (UNESP)-
Autor(es): dc.contributorRUDN University-
Autor(es): dc.contributorNational Institute for Space Research-
Autor(es): dc.contributorUniversitat Politècnica de Catalunya-
Autor(es): dc.creatorFormiga, Jorge Kennety Silva-
Autor(es): dc.creatordos Santos, Denilson Paulo Souza-
Autor(es): dc.creatorde Almeida Prado, Antonio Fernando Bertachini-
Autor(es): dc.creatorde Moraes, Rodolpho Vilhena-
Autor(es): dc.creatorDiaz, Julian Arnaldo Avila-
Data de aceite: dc.date.accessioned2025-08-21T15:18:57Z-
Data de disponibilização: dc.date.available2025-08-21T15:18:57Z-
Data de envio: dc.date.issued2025-04-29-
Data de envio: dc.date.issued2023-11-30-
Fonte completa do material: dc.identifierhttp://dx.doi.org/10.1140/epjs/s11734-023-01023-z-
Fonte completa do material: dc.identifierhttps://hdl.handle.net/11449/301473-
Fonte: dc.identifier.urihttp://educapes.capes.gov.br/handle/11449/301473-
Descrição: dc.descriptionSpace debris events are increasingly frequent where they are sufficiently dense that the use of low Earth orbit space has now reached the point under the effect of mutual collisions. As a mitigation method, the goal was to study the efficiency of an orbital maneuver considering the gravitational effect and ground-based laser when the space debris traveling in a heliocentric orbit in the range of 1 cm to 10 cm and altitude ranging from 100 to 1000 km makes a close approach to Earth. An analytical model was performed considering factors, such as the laser’s fluency, the debris’s inclination, and the relative movement between laser and debris. The analysis was performed through the variation of velocity and energy after a close approach considering a single pulse laser. It is important in evaluating the orbital characteristics of space debris for better reentry of Earth’s atmosphere or avoiding collisions considering the impulse magnitude performed by ground-based laser. Some results show that the laser can perform a small change in Δ V and have maximum efficiency in energy variation of 12 % that can be accumulated and perform energy of the reentry. In that sense, this study provides the literature with a general study of this maneuver, showing its advantages over more traditional orbital maneuvers, as well as the best conditions to avoid collisions and mitigate space debris.-
Descrição: dc.descriptionConselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)-
Descrição: dc.descriptionFundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)-
Descrição: dc.descriptionFederal State Budget Scientific Institution Research Institute - Republican Research and Consulting Center of Expertise-
Descrição: dc.descriptionEnvironmental Engineering Department São Paulo State University (UNESP) Institute of Science and Technology, SP-
Descrição: dc.descriptionAeronautical Engineering Department São Paulo State University UNESP-FESJ, São João da Boa Vista, 1387-
Descrição: dc.descriptionAcademy of Engineering RUDN University-
Descrição: dc.descriptionSpace Mechanical and Control National Institute for Space Research, SP-
Descrição: dc.descriptionDepartment of Strength of Materials and Structural Engineering-Barcelona School of Engineering (ETSEIB) Universitat Politècnica de Catalunya, Barcelona-
Descrição: dc.descriptionEnvironmental Engineering Department São Paulo State University (UNESP) Institute of Science and Technology, SP-
Descrição: dc.descriptionAeronautical Engineering Department São Paulo State University UNESP-FESJ, São João da Boa Vista, 1387-
Descrição: dc.descriptionCNPq: 0527/18-
Descrição: dc.descriptionFAPESP: 2016/15675-
Descrição: dc.descriptionFAPESP: 2017/04643-4-
Descrição: dc.descriptionFAPESP: 2022/13228-9-
Descrição: dc.descriptionFederal State Budget Scientific Institution Research Institute - Republican Research and Consulting Center of Expertise: 202235-2-000-
Formato: dc.format3059-3072-
Idioma: dc.languageen-
Relação: dc.relationEuropean Physical Journal: Special Topics-
???dc.source???: dc.sourceScopus-
Título: dc.titleGround-based laser effect on space debris maneuvering-
Tipo de arquivo: dc.typevídeo-
Aparece nas coleções:Repositório Institucional - Unesp

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