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1. Identity statement
Reference TypeJournal Article
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Siteplutao.sid.inpe.br (namespace prefix: upn:33M4QT8)
Identifier8JMKD3MGP3W/3UGCRGB
Repositorysid.inpe.br/plutao/2019/12.03.13.57.09   (restricted access)
Last Update2019:12.05.17.40.09 (UTC) lattes
Metadata Repositorysid.inpe.br/plutao/2019/12.03.13.57.10
Metadata Last Update2021:07.28.22.22.44 (UTC) administrator
DOI10.1088/1742-6596/1365/1/012008
ISSN1742-6588
Labellattes: 7340081273816424 3 FerreiraMoraPradWint:2019:EfMaPa
Citation KeyFerreiraMoraPradWint:2019:EfMaPa
TitleEffects of the mass parameter in the optimum direction of impulse and energy variation in a Powered Swing-By
Year2019
Access Date2026, Oct. 24
Type of Workconference paper
Secondary TypePRE PI
Number of Files1
Size977 KiB
2. Context
Author1 Ferreira, A. F. S.
2 Moraes, R. V.
3 Prado, Antonio Fernando Bertachini de Almeida
4 Winter, O. C.
Resume Identifier1
2
3 8JMKD3MGP5W/3C9JGJA
Group1
2
3 DIDMC-CGETE-INPE-MCTIC-GOV-BR
Affiliation1 Universidade Estadual Paulista (UNESP)
2
3 Instituto Nacional de Pesquisas Espaciais (INPE)
4 Universidade Estadual Paulista (UNESP)
Author e-Mail Address1 aleferrazsilva@hotmail.com
2
3 antonio.prado@inpe.br
JournalJournal of Physics: Conference Series
Volume1365
Pages012008
Secondary MarkB2_INTERDISCIPLINAR B2_ENGENHARIAS_III B3_MEDICINA_II B3_GEOCIÊNCIAS B4_MATERIAIS B4_ENGENHARIAS_II B4_BIOTECNOLOGIA C_QUÍMICA C_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA C_ENGENHARIAS_IV C_ECONOMIA C_ASTRONOMIA_/_FÍSICA
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01 upn:33M4QT8
History (UTC)2019-12-03 13:57:10 :: lattes -> administrator ::
2019-12-05 17:38:52 :: administrator -> lattes :: 2019
2019-12-05 17:40:11 :: lattes -> administrator :: 2019
2021-07-28 22:22:44 :: administrator -> simone :: 2019
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsAstrodinâmica
Astrodynamics
Swing-By
Manobras Orbitais
AbstractThe energy of a spacecraft, relative to the primary body of the system, before and after a Powered Swing-By maneuver with an impulse applied during the close encounter with the secondary body is studied. The Powered Swing-By maneuver is a combination of the effect of the gravity of a celestial body and an impulse applied to the spacecraft during its passage by the periapsis of its orbit relative to the secondary body. This combination modifies the spacecraft's trajectory, changing its parameters and, consequently, its energy. The objective is to quantify the effect of different mass parameters on the optimum direction to apply the impulse and in the energy variation of this more complex maneuver. It is focused on the twodimensional and elliptical maneuver. Optimum solutions for energy gains are presented.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Effects of the...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languagept
Target Fileferreira_effects.pdf
User Grouplattes
Reader Groupadministrator
lattes
Visibilityshown
Archiving Policydenypublisher denyfinaldraft12
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 - 106
sid.inpe.br/mtc-m21/2012/07.13.14.40.20 - 17
DisseminationWEBSCI; PORTALCAPES; COMPENDEX.
6. Notes
NotesXIX Brazilian Colloquium on Orbital Dynamics 2018
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn lineage mark mirrorrepository month nextedition number orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url
7. Description control
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