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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34P/3MPQHJS
Repositorysid.inpe.br/mtc-m21b/2016/11.11.18.40   (restricted access)
Last Update2016:11.11.18.40.30 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21b/2016/11.11.18.40.30
Metadata Last Update2021:07.28.22.52.23 (UTC) administrator
DOI10.1007/s40314-015-0287-3
ISSN2238-3603
Citation KeySantanaMeloMacaWint:2016:ExMoGr
TitleExploring the Moon gravity to escape from the Earth-Moon system
Year2016
MonthOct.
Access Date2024, June 13
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size1323 KiB
2. Context
Author1 Santana, Saymon Henrique Santos
2 Melo, Cristiano Fiorilo de
3 Macau, Elbert Einstein Nehrer
4 Winter, Othon Cabo
Resume Identifier1
2
3 8JMKD3MGP5W/3C9JGUT
Group1 CAP-COMP-SPG-INPE-MCTI-GOV-BR
2
3 LAC-CTE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Universidade Federal do ABC (UFABC)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
4 Universidade Estadual Paulista (UNESP)
Author e-Mail Address1 saymonhss@gmail.com
2
3 elbert.macau@inpe.br
4 ocwinter@gmail.com
JournalComputational and Applied Mathematics
Volume35
Number3
Pages701-710
History (UTC)2016-11-11 18:41:02 :: simone -> administrator :: 2016
2021-07-28 22:52:23 :: administrator -> simone :: 2016
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsSwing-by
Escape trajectories
Numerical simulations
AbstractEscape trajectories from the Earth-Moon system can be obtained through a single gravity assist maneuver of a spacecraft with the Moon. This paper presents a semi-analytical study of variations in the semi-major axis and the eccentricity of a spacecraft for a geocentric frame-before and after a close encounter of the spacecraft with the Moon. Studies on the swing-by dynamics between a spacecraft and the Moon were performed in order to establish a set of initial conditions in terms of eccentricities and semi-major axes of geocentric initial orbits. This way, it was possible identify which orbits, launched from Earth parking orbits, accomplish swing-bys with the Moon and generate escape trajectories.
AreaCOMP
Arrangement 1urlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABAC > Exploring the Moon...
Arrangement 2urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CAP > Exploring the Moon...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Content
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4. Conditions of access and use
Languageen
Target Filesantana_exploring.pdf
User Groupsimone
Reader Groupadministrator
simone
Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryurlib.net/www/2011/03.29.20.55
Next Higher Units8JMKD3MGPCW/3ESGTTP
8JMKD3MGPCW/3F2PHGS
Citing Item Listsid.inpe.br/bibdigital/2013/10.12.22.16 3
sid.inpe.br/mtc-m21/2012/07.13.14.45.07 2
sid.inpe.br/bibdigital/2013/09.22.23.14 1
DisseminationWEBSCI; PORTALCAPES; SCOPUS.
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
Empty Fieldsalternatejournal archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype url
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