1. Identity statement | |
Reference Type | Journal Article |
Site | mtc-m21c.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 8JMKD3MGP3W34R/42LA6JE |
Repository | sid.inpe.br/mtc-m21c/2020/06.10.15.29 (restricted access) |
Last Update | 2020:06.10.15.29.53 (UTC) simone |
Metadata Repository | sid.inpe.br/mtc-m21c/2020/06.10.15.29.53 |
Metadata Last Update | 2022:01.04.01.35.12 (UTC) administrator |
DOI | 10.1140/epjst/e2020-900144-9 |
ISSN | 1951-6355 |
Citation Key | MurciaPiñerosGomeDosSGole:2020:EfRoSp |
Title | Effects of the rotation of a spacecraft in an atmospheric close approach with the Earth |
Year | 2020 |
Month | May |
Access Date | 2024, May 02 |
Type of Work | journal article |
Secondary Type | PRE PI |
Number of Files | 1 |
Size | 1828 KiB |
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2. Context | |
Author | 1 Murcia Piñeros, Jhonathan Orlando 2 Gomes, Vivian Martins 3 Dos Santos, Walter Abrahão 4 Golebiewska, Justyna |
Resume Identifier | 1 2 3 8JMKD3MGP5W/3C9JJC2 |
Group | 1 DIDEA-CGETE-INPE-MCTIC-GOV-BR 2 3 DIDEA-CGETE-INPE-MCTIC-GOV-BR |
Affiliation | 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Universidade Estadual Paulista (UNESP) 3 Instituto Nacional de Pesquisas Espaciais (INPE) 4 Adam Mickiewicz University |
Author e-Mail Address | 1 jhonathan.pineros@inpe.br 2 vivianmartinsgomes@gmail.com 3 walter.abrahao@inpe.br |
Journal | European Physical Journal Special Topics |
Volume | 229 |
Number | 8 |
Pages | 1517-1526 |
History (UTC) | 2020-06-10 15:30:26 :: simone -> administrator :: 2020 2022-01-04 01:35:12 :: administrator -> simone :: 2020 |
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3. Content and structure | |
Is the master or a copy? | is the master |
Content Stage | completed |
Transferable | 1 |
Content Type | External Contribution |
Version Type | publisher |
Abstract | A maneuver called "Aerogravity Assisted" is known in the literature to increase the energy gains given by a close approach between a spacecraft and a planet using the atmosphere of the planet. Several previous papers showed the importance of this topic in different aspects. The present paper has the goal of studying the effects of the spacecraft rotation in this maneuver. This rotation implies in a variable ballistic coefficient and this fact can change the results of the maneuver. Several masses, sizes and angular velocities will be tested and the effects of these parameters will be measured. The dynamical model considers the atmosphere of the Earth, in terms of drag, the gravitational fields of the Earth and the Sun, assumed to be points of mass, and the rotating spacecraft. The Earth and the Sun are assumed to be in circular coplanar orbits around their common center of mass. The equations of motion are the ones given by the circular planar restricted three-body problem with the addition of the forces generated by the atmospheric drag. The primary objective is to map the energy variations of the spacecraft orbits due to this close approach as a function of the spacecraft angular velocity. This rotation can be used as control of the maneuver to try to reach different goals. |
Area | ETES |
Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDEA > Effects of the... |
doc Directory Content | access |
source Directory Content | there are no files |
agreement Directory Content | |
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4. Conditions of access and use | |
Language | en |
Target File | murica_effects.pdf |
User Group | simone |
Reader Group | administrator simone |
Visibility | shown |
Archiving Policy | denypublisher denyfinaldraft12 |
Read Permission | deny from all and allow from 150.163 |
Update Permission | not transferred |
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5. Allied materials | |
Next Higher Units | 8JMKD3MGPCW/3F6GF6B |
Citing Item List | sid.inpe.br/mtc-m21/2012/07.13.15.01.48 1 sid.inpe.br/bibdigital/2013/11.04.22.00 1 |
Dissemination | PORTALCAPES; SCOPUS. |
Host Collection | urlib.net/www/2017/11.22.19.04 |
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6. Notes | |
Empty Fields | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn keywords label lineage mark mirrorrepository nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype url |
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7. Description control | |
e-Mail (login) | simone |
update | |
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