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1. Identity statement
Reference TypeJournal Article
Sitemtc-m16b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier6qtX3pFwXQZGivnK2Y/QzKok
Repositorysid.inpe.br/mtc-m17@80/2007/06.27.19.03   (restricted access)
Last Update2007:06.27.19.03.52 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m17@80/2007/06.27.19.03.53
Metadata Last Update2018:06.05.03.34.26 (UTC) administrator
Secondary KeyINPE--PRE/
ISSN0273-1177
Citation KeyMeloMacaWintViei:2007:AlPaIn
TitleAlternative paths for insertion of probes into high inclination lunar orbits
Year2007
Access Date2024, May 19
Secondary TypePRE PI
Number of Files1
Size929 KiB
2. Context
Author1 Melo, Cristiano Fiorilo de
2 Macau, Elbert Einstein Nehrer
3 Winter, O. C.
4 Vieira Neto, E.
Resume Identifier1
2 8JMKD3MGP5W/3C9JGUT
Group1 LAC-INPE-MCT-BR
2 CRC-INPE-MCT-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Grupo de Dinâmica Orbital e Planetologia (UNESP)
4 Grupo de Dinâmica Orbital e Planetologia (UNESP)
JournalAdvances in Space Research
VolumeIn press
History (UTC)2007-12-19 16:24:37 :: simone -> administrator ::
2012-07-13 22:23:04 :: administrator -> simone ::
2012-10-03 14:29:11 :: simone -> administrator :: 2007
2012-10-28 03:50:48 :: administrator -> banon :: 2007
2013-02-19 13:56:17 :: banon -> simone :: 2007
2013-02-20 15:20:00 :: simone -> administrator :: 2007
2018-06-05 03:34:26 :: administrator -> marciana :: 2007
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsAstrodynamics
Mission design
Earth-Moon transfer
Orbital maneuvers
AbstractThe dynamics of the restricted three-body Earth-Moon-particle problem predicts the existence of direct periodic orbits around the Lagrangian equilibrium point L1. From these orbits, we derive a set of trajectories that form links between the Earth and the Moon and are capable of performing transfers between terrestrial and lunar orbits, in addition to defining an escape route from the Earth-Moon system. When we consider a more complex and realistic dynamical system - the four-body Sun-Earth-Moon-particle (probe) problem - the trajectories have an expressive gain of inclination when they penetrate in the lunar influence sphere, thus allowing the insertion of probes into low-altitude lunar orbits with high inclinations, including polar orbits. In this study, we present these links and investigate some possibilities for performing an Earth-Moon transfer based on these trajectories.
AreaCOMP
Arrangement 1urlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABAC > Alternative paths for...
Arrangement 2urlib.net > COCRC > Alternative paths for...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target FileAlternative paths.pdf
User Groupadministrator
banon
simone
Reader Groupadministrator
simone
Visibilityshown
Archiving Policydenypublisher denyfinaldraft24
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/3ESGTTP
8JMKD3MGPCW/3F3PAJE
Citing Item Listsid.inpe.br/bibdigital/2013/10.19.00.29 1
sid.inpe.br/mtc-m21/2012/07.13.14.45.07 1
DisseminationWEBSCI; PORTALCAPES; MGA; COMPENDEX.
Host Collectionlcp.inpe.br/ignes/2004/02.12.18.39
cptec.inpe.br/walmeida/2003/04.25.17.12
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel doi e-mailaddress electronicmailaddress format isbn label lineage mark mirrorrepository month nextedition notes number orcid pages parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url
7. Description control
e-Mail (login)marciana
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