1. Identity statement | |
Reference Type | Journal Article |
Site | mtc-m21b.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 8JMKD3MGP3W34P/3MPQHJS |
Repository | sid.inpe.br/mtc-m21b/2016/11.11.18.40 (restricted access) |
Last Update | 2016:11.11.18.40.30 (UTC) administrator |
Metadata Repository | sid.inpe.br/mtc-m21b/2016/11.11.18.40.30 |
Metadata Last Update | 2021:07.28.22.52.23 (UTC) administrator |
DOI | 10.1007/s40314-015-0287-3 |
ISSN | 2238-3603 |
Citation Key | SantanaMeloMacaWint:2016:ExMoGr |
Title | Exploring the Moon gravity to escape from the Earth-Moon system |
Year | 2016 |
Month | Oct. |
Access Date | 2024, May 19 |
Type of Work | journal article |
Secondary Type | PRE PI |
Number of Files | 1 |
Size | 1323 KiB |
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2. Context | |
Author | 1 Santana, Saymon Henrique Santos 2 Melo, Cristiano Fiorilo de 3 Macau, Elbert Einstein Nehrer 4 Winter, Othon Cabo |
Resume Identifier | 1 2 3 8JMKD3MGP5W/3C9JGUT |
Group | 1 CAP-COMP-SPG-INPE-MCTI-GOV-BR 2 3 LAC-CTE-INPE-MCTI-GOV-BR |
Affiliation | 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Universidade Federal do ABC (UFABC) 3 Instituto Nacional de Pesquisas Espaciais (INPE) 4 Universidade Estadual Paulista (UNESP) |
Author e-Mail Address | 1 saymonhss@gmail.com 2 3 elbert.macau@inpe.br 4 ocwinter@gmail.com |
Journal | Computational and Applied Mathematics |
Volume | 35 |
Number | 3 |
Pages | 701-710 |
History (UTC) | 2016-11-11 18:41:02 :: simone -> administrator :: 2016 2021-07-28 22:52:23 :: administrator -> simone :: 2016 |
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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 |
Keywords | Swing-by Escape trajectories Numerical simulations |
Abstract | Escape trajectories from the Earth-Moon system can be obtained through a single gravity assist maneuver of a spacecraft with the Moon. This paper presents a semi-analytical study of variations in the semi-major axis and the eccentricity of a spacecraft for a geocentric frame-before and after a close encounter of the spacecraft with the Moon. Studies on the swing-by dynamics between a spacecraft and the Moon were performed in order to establish a set of initial conditions in terms of eccentricities and semi-major axes of geocentric initial orbits. This way, it was possible identify which orbits, launched from Earth parking orbits, accomplish swing-bys with the Moon and generate escape trajectories. |
Area | COMP |
Arrangement 1 | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABAC > Exploring the Moon... |
Arrangement 2 | urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CAP > Exploring the Moon... |
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 | santana_exploring.pdf |
User Group | simone |
Reader Group | administrator simone |
Visibility | shown |
Read Permission | deny from all and allow from 150.163 |
Update Permission | not transferred |
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5. Allied materials | |
Mirror Repository | urlib.net/www/2011/03.29.20.55 |
Next Higher Units | 8JMKD3MGPCW/3ESGTTP 8JMKD3MGPCW/3F2PHGS |
Citing Item List | sid.inpe.br/bibdigital/2013/10.12.22.16 3 sid.inpe.br/mtc-m21/2012/07.13.14.45.07 1 sid.inpe.br/bibdigital/2013/09.22.23.14 1 |
Dissemination | WEBSCI; PORTALCAPES; SCOPUS. |
Host Collection | sid.inpe.br/mtc-m21b/2013/09.26.14.25.20 |
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6. Notes | |
Empty Fields | alternatejournal archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark 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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