| 1. Identificação | ||||
| Tipo de Referência | Artigo em Evento (Conference Proceedings) | |||
| Site | mtc-m21d.sid.inpe.br | |||
| Código do Detentor | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S | |||
| Identificador | 8JMKD3MGP3W34T/47LCMPP | |||
| Repositório | sid.inpe.br/mtc-m21d/2022/09.19.14.32 | |||
| Última Atualização | 2022:09.19.14.32.18 (UTC) simone | |||
| Repositório de Metadados | sid.inpe.br/mtc-m21d/2022/09.19.14.32.18 | |||
| Última Atualização dos Metadados | 2023:01.03.16.46.16 (UTC) administrator | |||
| Chave Secundária | INPE--PRE/ | |||
| Chave de Citação | RaoSRWWLJMOLS:2022:MeSaRe | |||
| Título | Mercury sample return mission design utilizing innovative systems and technologies  | |||
| Ano | 2022 | |||
| Data de Acesso | 11 maio 2024 | |||
| Tipo Secundário | PRE CI | |||
| Número de Arquivos | 1 | |||
| Tamanho | 38 KiB | |||
| 2. Contextualização | ||||
| Autor | 1 Rao, Sapna 2 Sinha, Priyanka 3 Rojas Ramirez, Marcos Edoardo 4 Winter, Bram de 5 Williams, Saira O. 6 Landers, Viduranga 7 Jagadam, Nitya 8 Morchedi, Sondes 9 Oseni, Dorcas Dupe 10 Laabidi, Rayen 11 Singh, Harsh | |||
| Grupo | 1 2 3 4 5 6 7 8 9 GESAST-CEA-DIPGR-INPE-MCTI-GOV-BR | |||
| Afiliação | 1 Lockheed Martin (Space Systems Company) 2 Israel Institute of Technology 3 Institut Supérieur de l’Aéronautique et de l’Espace (ISAE) 4 Space Generation Advisory Council (SGAC) 5 Space Generation Advisory Council (SGAC) 6 Nexus Aurora 7 Space Generation Advisory Council (SGAC) 8 Universität der Bundeswehr München 9 Instituto Nacional de Pesquisas Espaciais (INPE) 10 Space Generation Advisory Council (SGAC) 11 University of Petroleum and Energy Studies | |||
| Endereço de e-Mail do Autor | 1 sapna.rao@lmco.com 2 sinhapriyankanepal@gmail.com 3 Marcos-eduardo.Rojas-Ramirez@isae-supaero.fr 4 bram.dewinter@spacegeneration.org 5 roxysairawilliams@spacegeneration.org 6 vidurangalanders@gmail.com 7 jagadamnitya@gmail.com 8 sondesmorchedi@gmail.com 9 dorcasdupe16@gmail.com 10 rayenlaabidi@gmail.com 11 harsh.singh2000@gmail.com | |||
| Nome do Evento | International Astronautical Congress, 73 | |||
| Localização do Evento | Paris, France | |||
| Data | 18-22 Sept. 2022 | |||
| Editora (Publisher) | IAF | |||
| Histórico (UTC) | 2022-09-19 14:32:18 :: simone -> administrator :: 2023-01-03 16:46:16 :: administrator -> simone :: 2022 | |||
| 3. Conteúdo e estrutura | ||||
| É a matriz ou uma cópia? | é a matriz | |||
| Estágio do Conteúdo | concluido | |||
| Transferível | 1 | |||
| Tipo do Conteúdo | External Contribution | |||
| Resumo | Mercury is one of four terrestrial planets and the smallest planet in the solar system, known to have a significant metallic core and a high metal to silicate ratio. However, the reason for the planets specific composition and formation is yet to be explained. While many theories attempt to justify these facts, none can be confirmed without further investigation, such as one provided by a sample return mission. The science collected from this mission will allow for validation of theories about the formation of Mercury and possibly the Solar System. By investigating theories about Mercurys formation, more information will be uncovered about the Earths Moon as there are quite a few similarities between the two bodies. These similarities will help establish a newer, more grounded theory about the origin of the Moon and its effects on Earth. Additionally, learning about Mercury could provide information on how the Earth might evolve over time. Sending a spacecraft to Mercury has many challenges, orbital mechanics being one of the biggest. As Mercury is the closest planet to the Sun, its orbit is the most affected by the Suns gravity, making it difficult to maneuver a spacecraft into a stable orbit. Moreover, going to Mercury is a complicated and long-duration mission requiring gravity assists and complex trajectories. Thermal control is another challenge since the spacecraft must be protected from Mercurys extreme temperatures. In this context, this research will attempt to deal with these difficulties through innovative analyses of technologies to develop a feasible plan to perform such a mission. The study will present trades of different technologies and approaches for subsystems. Due to the previously discussed challenges imposed by Mercury, employing an innovative approach to the technologies will allow for designing a mission optimal for combatting challenges. The paper will also discuss the mission design tools and Model-Based Systems Engineering (MBSE) approaches used to validate results. Please note that this work is submitted under the guidance of the Space Exploration Project Group (SEPG) of the Space Generation Advisory Council (SGAC) as part of the ACHIEVED Initiative, which stands for Assembly for Concepts in Human Interplanetary Exploration with Various Extraterrestrial Designations. This initiative aims to enable students and young professionals from diverse technical and cultural backgrounds to work and collaborate on a space mission design project. | |||
| Área | CEA | |||
| Arranjo 1 | urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > GES > Mercury sample return... | |||
| Arranjo 2 | urlib.net > BDMCI > Fonds > Produção a partir de 2021 > CGCE > Mercury sample return... | |||
| Conteúdo da Pasta doc | acessar | |||
| Conteúdo da Pasta source | não têm arquivos | |||
| Conteúdo da Pasta agreement |
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| 4. Condições de acesso e uso | ||||
| URL dos dados | http://urlib.net/ibi/8JMKD3MGP3W34T/47LCMPP | |||
| URL dos dados zipados | http://urlib.net/zip/8JMKD3MGP3W34T/47LCMPP | |||
| Idioma | en | |||
| Arquivo Alvo | IAC-22,A3,5,1,x69552.brief.pdf | |||
| Grupo de Usuários | simone | |||
| Visibilidade | shown | |||
| Permissão de Atualização | não transferida | |||
| 5. Fontes relacionadas | ||||
| Unidades Imediatamente Superiores | 8JMKD3MGPCW/3F2PBEE 8JMKD3MGPCW/46KTFK8 | |||
| Lista de Itens Citando | sid.inpe.br/bibdigital/2013/10.12.21.02 2 | |||
| Acervo Hospedeiro | urlib.net/www/2021/06.04.03.40 | |||
| 6. Notas | ||||
| Campos Vazios | archivingpolicy archivist booktitle callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor format isbn issn keywords label lineage mark mirrorrepository nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisheraddress readergroup readpermission resumeid rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url versiontype volume | |||
| 7. Controle da descrição | ||||
| e-Mail (login) | simone | |||
| atualizar | ||||