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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21d.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34T/47CHHUH
Repositorysid.inpe.br/mtc-m21d/2022/08.02.12.07   (restricted access)
Last Update2022:08.02.12.07.43 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21d/2022/08.02.12.07.43
Metadata Last Update2023:01.03.16.46.11 (UTC) administrator
DOI10.1016/j.asr.2022.05.031
ISSN0273-1177
1879-1948
Citation KeyMurciaPiñerosMoraPrad:2022:UsLoLi
TitleUsing low Lift-to-Drag spacecraft to perform upper atmospheric Aero-Gravity Assisted Maneuvers
Year2022
MonthAug.
Access Date2024, May 13
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size2430 KiB
2. Context
Author1 Murcia Piñeros, Jhonathan O.
2 Moraes, Rodolpho Vilhena de
3 Prado, Antonio Fernando Bertachini de Almeida
Resume Identifier1
2
3 8JMKD3MGP5W/3C9JGJA
Group1
2
3 DIMEC-CGCE-INPE-MCTI-GOV-BR
Affiliation1 Universidade Estadual Paulista (UNESP)
2 Universidade Estadual Paulista (UNESP)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 jhonathan.pineros@unifesp.br
2 rodolpho.vilhena@gmail.com
3 antonio.prado@inpe.br
JournalAdvances in Space Research
Volume70
Number4
Pages1032-1047
Secondary MarkB1_INTERDISCIPLINAR B1_GEOCIÊNCIAS B1_ENGENHARIAS_IV B1_ENGENHARIAS_III B1_BIODIVERSIDADE B3_CIÊNCIA_DA_COMPUTAÇÃO B4_ASTRONOMIA_/_FÍSICA C_CIÊNCIAS_BIOLÓGICAS_I
History (UTC)2022-08-02 12:07:43 :: simone -> administrator ::
2022-08-02 12:07:43 :: administrator -> simone :: 2022
2022-08-02 12:07:56 :: simone -> administrator :: 2022
2023-01-03 16:46:11 :: administrator -> simone :: 2022
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsAerodynamic forces
Astrodynamics
Atmosphere
Interplanetary flight
Orbit propagation
Spacecraft maneuvers
Swing-by
AbstractThe Gravity Assisted Maneuver has been applied in lots of space missions, to change the spacecraft heliocentric velocity vector and the geometry of the orbit, after the close approach to a celestial body, saving propellant consumption. It is possible to take advantage of additional forces to improve the maneuver, like the forces generated by the spacecraft-atmosphere interaction and/or propulsion systems; reducing the time of flight and the need for multiple passages around secondary bodies. However, these applications require improvements in critical subsystems, which are necessary to accomplish the mission. In this paper, a few combinations of the Gravity-Assist were classified, including maneuvers with thrust and aerodynamic forces; presenting the advantages and limitations of these variations. There are analyzed the effects of implementing low Lift-to-Drag ratios at high altitudes for Aero-gravity Assist maneuvers, with and without propulsion. The maneuvers were simulated for Venus and Mars, due to their relevance in interplanetary missions, the interest in exploration, and the knowledge about their atmospheres. The Aero-gravity Assist maneuver with low Lift-to-Drag ratios at high altitudes shows an increase of more than 10° in the turn angle for Venus and 2.5° for Mars. The maneuvers increase the energy gains by more than 15% when compared to the Gravity-Assist. From the Technology Readiness Levels, it was observed that the current level of development of the space technology makes feasible the application of Aero-gravity Assisted Maneuvers at high altitudes in short term.
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4. Conditions of access and use
Languageen
Target File1-s2.0-S0273117722004100-main.pdf
User Groupsimone
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/46KTFK8
DisseminationWEBSCI; PORTALCAPES; COMPENDEX; SCOPUS.
Host Collectionurlib.net/www/2021/06.04.03.40
6. Notes
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