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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Siteplutao.sid.inpe.br (namespace prefix: upn:33M4QT8)
Identifier8JMKD3MGP3W/3FCL5QH
Repositorysid.inpe.br/plutao/2013/12.12.15.43
Last Update2014:01.17.12.19.11 (UTC) administrator
Metadata Repositorysid.inpe.br/plutao/2013/12.12.15.43.14
Metadata Last Update2021:02.11.18.16.25 (UTC) administrator
ISBN978-1-61804-194-4
Labellattes: 7340081273816424 1 Prado:2013:SwCoIm
Citation KeySilvaPradWint:2013:SwCoIm
TitleSwing-By Combined with Impulsive Maneuvers in the Sun-Jupiter System
FormatPapel
Year2013
Access Date2026, Oct. 07
Secondary TypePRE CI
Number of Files1
Size589 KiB
2. Context
Author1 Silva, Alessandra Ferraz da
2 Prado, Antonio Fernando Bertachini de Almeida
3 Winter, Othon Cabo
Resume Identifier1
2 8JMKD3MGP5W/3C9JGJA
Group1
2 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Grupo de Dinâmica Orbital & Planetologia – Univ. Estadual Paulista - UNESP – Brazil
e-Mail Addressantonio.prado@inpe.br
Conference NameInternational Conference on Mathematical Models for Engineering Science, 4.
Conference LocationBrasov
Book TitleProceedings
Tertiary TypePaper
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01 upn:33M4QT8
History (UTC)2013-12-12 15:43:14 :: lattes -> administrator ::
2014-01-15 18:59:51 :: administrator -> marcelo.pazos@sid.inpe.br :: 2013
2014-01-17 12:19:11 :: marcelo.pazos@sid.inpe.br -> administrator :: 2013
2021-02-11 18:16:25 :: administrator -> marcelo.pazos@inpe.br :: 2013
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
KeywordsSwing-By
impulsive maneuver
spacecraft trajectories
AbstractThis paper makes a study of the effects of a Swing-By combined with an impulsive maneuver in the orbit of a spacecraft passing by Jupiter in the Sun-Jupiter system. The Swing-By is a maneuver where the spacecraft approaches a celestial body to gain or lose energy from its gravity. This combined maneuver causes a change in the orbit of the spacecraft. The goal is to calculate the maximum variation of the energy obtained from this combined maneuver. This type of maneuver is important, because it generates a significant fuel economy in space missions. The studies were done with the periapse of the orbit of the spacecraft around Jupiter in different points and with the impulse applied in different directions. The results show that, in general, the application of the impulse in directions that are not tangential to the orbit is more efficient.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Swing-By Combined with...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
data URIupn:33M4QT8:8JMKD3MGP3W/3FCL5QH
data URLhttp://urlib.net/ibi/8JMKD3MGP3W/3FCL5QH
zipped data URLhttp://urlib.net/zip/8JMKD3MGP3W/3FCL5QH
Languageen
Target FileMMIC-15.pdf
User Grouplattes
marcelo.pazos@inpe.br
Reader Groupadministrator
marcelo.pazos@inpe.br
Visibilityshown
Read Permissionallow from all
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryiconet.com.br/banon/2006/11.26.21.31
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 - 69
sid.inpe.br/bibdigital@80/2006/12.20.14.49 - 12
sid.inpe.br/mtc-m21/2012/07.13.14.40.20 - 10
sid.inpe.br/bibdigital@80/2006/04.07.15.50.13 - 7
sid.inpe.br/mtc-m21/2012/06.05.15.34.41 - 6
6. Notes
Empty Fieldsarchivingpolicy archivist callnumber copyholder copyright creatorhistory date descriptionlevel dissemination doi edition editor electronicmailaddress issn lineage mark nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress rightsholder schedulinginformation secondarydate secondarykey secondarymark serieseditor session shorttitle sponsor subject tertiarymark type url versiontype volume
7. Description control
e-Mail (login)marcelo.pazos@inpe.br
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