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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21c.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34R/3SKLETB
Repositorysid.inpe.br/mtc-m21c/2019/01.25.14.48   (restricted access)
Last Update2019:01.25.14.48.05 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21c/2019/01.25.14.48.05
Metadata Last Update2021:07.28.22.52.25 (UTC) administrator
DOI10.1007/s40314-017-0525-y
ISSN2238-3603
Citation KeyCarvalhoSantPradMora:2018:SoChOr
TitleSome characteristics of orbits for a spacecraft around Mercury
Year2018
MonthDec.
Access Date2024, May 08
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size3242 KiB
2. Context
Author1 Carvalho, Jean Paulo S.
2 Santos, J. Cardoso dos
3 Prado, Antonio Fernando Bertachini de Almeida
4 Moraes, R. Vilhena de
Resume Identifier1
2
3 8JMKD3MGP5W/3C9JGJA
ORCID1 0000-0002-1979-3739
Group1
2
3 DIDMC-CGETE-INPE-MCTIC-GOV-BR
Affiliation1 Universidade Federal do Reconcavo da Bahia (UFRB)
2 Universidade Estadual Paulista (UNESP)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
4 Universidade Federal de São Paulo (UNIFESP)
Author e-Mail Address1
2
3 antonio.prado@inpe.br
JournalComputational and Applied Mathematics
Volume37
NumberSuppl. 1
Pages267-281
Secondary MarkB2_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA B2_INTERDISCIPLINAR B3_CIÊNCIA_DA_COMPUTAÇÃO B4_ENGENHARIAS_IV
History (UTC)2019-01-25 14:49:01 :: simone -> administrator :: 2018
2021-07-28 22:52:25 :: administrator -> simone :: 2018
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsSolar sail
Frozen orbits
Third-body perturbation
Solar radiation pressure
Mercury
AbstractSolar sails are a type of propulsion that uses solar radiation pressure to generate acceleration. The fundamental goal for any solar sail design is to provide a large and flat reflective film which requires a minimum of structural support mass. This research takes into account the non-sphericity of the central body, the perturbation of the third body and the solar radiation pressure to analyze the behavior of the orbit of a spacecraft when it has a solar sail around Mercury. We present an approach where we plot maps to analyze frozen orbits with longer lifetimes around Mercury. A set of initial conditions, which may contribute with the scientific missions planned to visit the planet Mercury in the next few years, are presented. Frozen orbits were found, i.e., orbits with smaller variation of the orbital elements. An approach is also presented to analyze the effect of the non-sphericity of Mercury on the motion of the spacecraft. In addition, the J2 and J3 zonal terms are also considered, as well as the C22 sectorial term.
AreaETES
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4. Conditions of access and use
Languageen
Target Filecarvalho_some.pdf
User Groupsimone
Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryurlib.net/www/2017/11.22.19.04.03
Next Higher Units8JMKD3MGPCW/446AF4B
DisseminationWEBSCI; PORTALCAPES; SCOPUS.
Host Collectionurlib.net/www/2017/11.22.19.04
6. Notes
Empty Fieldsalternatejournal archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark nextedition notes parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url
7. Description control
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