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1. Identity statement Reference Type Journal Article Site mtc-m21c.sid.inpe.br Holder Code isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S Identifier 8JMKD3MGP3W34R/3R3EN5E Repository sid.inpe.br/mtc-m21c/2018/05.04.19.41   (restricted access) Last Update 2018:05.04.19.41.12 (UTC) administrator Metadata Repository sid.inpe.br/mtc-m21c/2018/05.04.19.41.12 Metadata Last Update 2021:02.11.18.10.39 (UTC) administrator DOI 10.1007/s10509-018-3308-z ISSN 0004-640X Citation Key MouraJúniorCelePrad:2018:DeOpCo Title Determination of the optimal conditions for inclination maneuvers using a Swing-by Year 2018 Month may Access Date 2024, May 08 Type of Work journal article Secondary Type PRE PI Number of Files 1 Size 4185 KiB 2. Context Author 1 Moura Júnior, O. 2 Celestino, C. C. 3 Prado, Antonio Fernando Bertachini de Almeida Resume Identifier 1 2 3 8JMKD3MGP5W/3C9JGJA Group 1 2 3 DIDMC-CGETE-INPE-MCTIC-GOV-BR Affiliation 1 Universidade Federal do ABC (UFABC) 2 Universidade Federal do ABC (UFABC) 3 Instituto Nacional de Pesquisas Espaciais (INPE) Author e-Mail Address 1 osvaldomourajr@hotmail.com 2 3 antonio.prado@inpe.br Journal Astrophysics and Space Science Volume 363 Number 5 Pages e91 Secondary Mark B1_GEOCIÊNCIAS B3_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA B3_ASTRONOMIA_/_FÍSICA History (UTC) 2018-05-04 19:41:12 :: simone -> administrator :: 2018-05-04 19:41:12 :: administrator -> simone :: 2018 2018-05-04 19:42:14 :: simone -> administrator :: 2018 2021-02-11 18:10:39 :: administrator -> simone :: 2018 3. Content and structure Is the master or a copy? is the master Content Stage completed Transferable 1 Content Type External Contribution Version Type publisher Keywords Swing-by · Orbital maneuvers · Changing of orbital plane · Astrodynamics Abstract The search for methods to reduce the fuel consumption in orbital transfers is something relevant and always current in astrodynamics. Therefore, the maneuvers assisted by the gravity, also called Swing-by maneuvers, can be an advantageous option to save fuel. The proposal of the present research is to explore the influence of some parameters in a Swing-by of an artificial satellite orbiting a planet with one of the moons of this mother planet, with the goal of changing the inclination of the artificial satellite around the main body of the system. The fuel consumption of this maneuver is compared with the required consumption to perform the same change of inclination using the classical approach of impulsive maneuvers. Area ETES Arrangement urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Determination of the... doc Directory Content access source Directory Content there are no files agreement Directory Content agreement.html 04/05/2018 16:41 1.0 KiB  4. Conditions of access and use Language en User Group self-uploading-INPE-MCTI-GOV-BR simone Visibility shown Archiving Policy denypublisher denyfinaldraft12 Read Permission deny from all and allow from 150.163 Update Permission not transferred 5. Allied materials Linking Trabalho não Vinculado à Tese/Dissertação Next Higher Units 8JMKD3MGPCW/446AF4B Dissemination WEBSCI; PORTALCAPES. Host Collection urlib.net/www/2017/11.22.19.04 6. Notes Empty Fields alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark mirrorrepository nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject targetfile tertiarytype url 7. Description control e-Mail (login) simone update

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