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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP5W34M/3GD3GJU
Repositorysid.inpe.br/mtc-m21b/2014/05.30.02.23.05   (restricted access)
Last Update2014:07.16.18.53.20 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21b/2014/05.30.02.23.06
Metadata Last Update2018:06.04.03.04.15 (UTC) administrator
DOI10.1016/j.asr.2013.11.055
ISSN0273-1177
1879-1948
Labelscopus 2014-05 SalazarMacaWint:2014:AlTrEa
Citation KeySalazarMacaWint:2014:AlTrEa
TitleAlternative transfer to the Earth-Moon Lagrangian points L4 and L5 using lunar gravity assist
ProjectFapesp (2008/06066-5, 2011/08171-3, 2013/03233-6).
Year2014
Access Date2024, June 14
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size1944 KiB
2. Context
Author1 Salazar, F. J. T.
2 Macau, Elbert Einstein Nehrer
3 Winter, O. C.
Resume Identifier1
2 8JMKD3MGP5W/3C9JGUT
Group1
2 LAC-CTE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 UNESP, Grupo de Dinâmica Orbital e Planetologia, Guaratinguetá, SP 12516-410, Brazil
Author e-Mail Address1 e7940@hotmail.com
2 elbert.macau@inpe.br
3 ocwinter@gmail.com
e-Mail Addressmarcelo.pazos@inpe.br
JournalAdvances in Space Research
Volume53
Number3
Pages543-557
History (UTC)2018-06-04 03:04:15 :: administrator -> marcelo.pazos@inpe.br :: 2014
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsL4
L5
Lagrangian points
Patched-conic
Swing by
Three-body problem
Lagrange multipliers
Space stations
Trajectories
Moon
AbstractLagrangian points L4 and L5 lie at 60 ahead of and behind the Moon in its orbit with respect to the Earth. Each one of them is a third point of an equilateral triangle with the base of the line defined by those two bodies. These Lagrangian points are stable for the Earth-Moon mass ratio. As so, these Lagrangian points represent remarkable positions to host astronomical observatories or space stations. However, this same distance characteristic may be a challenge for periodic servicing mission. This paper studies elliptic trajectories from an Earth circular parking orbit to reach the Moon's sphere of influence and apply a swing-by maneuver in order to re-direct the path of a spacecraft to a vicinity of the Lagrangian points L4 and L5. Once the geocentric transfer orbit and the initial impulsive thrust have been determined, the goal is to establish the angle at which the geocentric trajectory crosses the lunar sphere of influence in such a way that when the spacecraft leaves the Moon's gravitational field, its trajectory and velocity with respect to the Earth change in order to the spacecraft arrives at L4 and L5. In this work, the planar Circular Restricted Three Body Problem approximation is used and in order to avoid solving a two boundary problem, the patched-conic approximation is considered.
AreaCOMP
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABAC > Alternative transfer to...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target File1-s2.0-S0273117713007588-main.pdf
User Groupadministrator
marcelo.pazos@inpe.br
Reader Groupadministrator
marcelo.pazos@inpe.br
Visibilityshown
Archiving Policydenypublisher denyfinaldraft24
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryiconet.com.br/banon/2006/11.26.21.31
Next Higher Units8JMKD3MGPCW/3ESGTTP
Citing Item Listsid.inpe.br/bibdigital/2013/09.22.23.14 4
sid.inpe.br/mtc-m21/2012/07.13.14.45.07 2
URL (untrusted data)http://dx.doi.org/10.1016/j.asr.2013.11.055
DisseminationWEBSCI; PORTALCAPES; COMPENDEX; SCOPUS.
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel format isbn lineage mark month nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype
7. Description control
e-Mail (login)marcelo.pazos@inpe.br
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