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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21d.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34T/47HEBLB
Repositorysid.inpe.br/mtc-m21d/2022/09.01.12.33   (restricted access)
Last Update2022:09.01.12.33.32 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21d/2022/09.01.12.33.32
Metadata Last Update2023:01.03.16.46.14 (UTC) administrator
DOI10.1038/s41598-022-15588-7
ISSN2045-2322
Citation KeyChagasPradWint:2022:GrPeCo
TitleGravitational perturbations correlated with the asteroid kinetic impact deflection technique
Year2022
MonthJuly
Access Date2024, May 14
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size6172 KiB
2. Context
Author1 Chagas, Bruno S.
2 Prado, Antonio Fernando Bertachini de Almeida
3 Winter, O. C.
Resume Identifier1
2 8JMKD3MGP5W/3C9JGJA
Group1
2 DIMEC-CGCE-INPE-MCTI-GOV-BR
Affiliation1 Universidade Estadual Paulista (UNESP)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Universidade Estadual Paulista (UNESP)
Author e-Mail Address1 bruno.chagas@unesp.br
2 antonio.prado@inpe.br
JournalScientific Reports
Volume12
Number1
Pagese11721
Secondary MarkB2_BIODIVERSIDADE B3_ODONTOLOGIA B3_LETRAS_/_LINGUÍSTICA C_CIÊNCIAS_BIOLÓGICAS_III C_BIOTECNOLOGIA C_ASTRONOMIA_/_FÍSICA
History (UTC)2022-09-01 12:33:51 :: simone -> administrator :: 2022
2023-01-03 16:46:14 :: administrator -> simone :: 2022
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
AbstractThis paper presents the use of the kinetic impact technique to deflect asteroids that may present some risk of collision with Earth. Within the work to be developed here, we intend to evaluate in more detail the possibility to deflect the orbit of the asteroid 101955 Bennu by applying variations in its velocity (Delta v) at different positions along its orbital period and measuring effects of close encounters with planet Earth. We will see that, in a relatively long period of time, the asteroid has several close encounters with the planet, thus suffering a natural gravitational perturbation. With the application of the impulses, the relative distances change, causing variations in the energy of the asteroid and a large variation in the relative distance between the asteroid and Earth over a long period after the impulse. We present results related to the magnitude of the impulse applied, which is important because its defines the mass and velocity of the impactor to be considered. Then, we mapped the positions of the impulses along a period of the orbit of the asteroid. We finish by explaining what happens to the orbit of the asteroid during the periods of gravitational perturbation, since the close encounters amount to "Swing Bys" that intensify the variations of the relative distances between the bodies after the impulse is applied.
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4. Conditions of access and use
Languageen
Target Files41598-022-15588-7.pdf
User Groupsimone
Reader Groupadministrator
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Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/46KTFK8
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.40.20 1
DisseminationWEBSCI; PORTALCAPES; SCOPUS.
Host Collectionurlib.net/www/2021/06.04.03.40
6. Notes
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