Close
Metadata

1. Identity statement
Reference TypeJournal Article
Sitemtc-m16d.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP7W/38UG29E
Repositorysid.inpe.br/mtc-m19/2011/01.12.14.26   (restricted access)
Last Update2011:02.02.17.09.58 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m19/2011/01.12.14.26.50
Metadata Last Update2021:02.11.18.10.28 (UTC) administrator
Secondary KeyINPE--PRE/
DOI10.1155/2010/313571
ISSN1024-123X
1563-5147
Citation KeyHuauraSolorzanoBertSukh:2010:OuPlMi
TitleOuter Planet Missions with Electric Propulsion Systems-Part I
Year2010
Access Date2024, May 05
Secondary TypePRE PI
Number of Files1
Size1251 KiB
2. Context
Author1 Huaura Solorzano, Carlos Renato
2 Bertachini de Almeida Prado, Antonio Fernando
3 Sukhanov, Alexander Alexandrovich
Resume Identifier1
2 8JMKD3MGP5W/3C9JGJA
Group1
2 DMC-ETE-INPE-MCT-BR
Affiliation1
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Space Research Institute (IKI) of the Russian Academy of Sciences, 84/32 Profsoyuznaya St., 117997 Moscow, Russia
JournalMathematical Problems in Engineering
VolumeArticle ID 313571
Secondary MarkB5_ASTRONOMIA_/_FÍSICA B4_CIÊNCIA_DA_COMPUTAÇÃO B3_CIÊNCIAS_AGRÁRIAS_I B1_ENGENHARIAS_I B2_ENGENHARIAS_II B1_ENGENHARIAS_III A2_ENGENHARIAS_IV A2_INTERDISCIPLINAR B3_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA
History (UTC)2011-12-19 13:28:27 :: marciana -> administrator :: 2010
2012-07-15 02:57:27 :: administrator -> marciana :: 2010
2013-03-01 13:09:06 :: marciana -> administrator :: 2010
2021-02-11 18:10:28 :: administrator -> marciana :: 2010
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
AbstractFor interplanetary missions, efficient electric propulsion systems can be used to increase the mass delivered to the destination. Outer planet exploration has experienced new interest with the launch of the Cassini and New Horizons Missions. At the present, new technologies are studied for better use of electric propulsion systems in missions to the outer planets. This paper presents low-thrust trajectories using the method of the transporting trajectory to Uranus, Neptune, and Pluto. They use nuclear and radio isotopic electric propulsion. These direct transfers have continuous electric propulsion of low power along the entire trajectory. The main goal of the paper is to optimize the transfers, that is, to provide maximum mass to be delivered to the outer planets.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Outer Planet Missions...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Content
agreement.html 12/01/2011 12:26 1.0 KiB 
4. Conditions of access and use
Languageen
Target File313571.pdf
User Groupadministrator
marciana
Visibilityshown
Archiving Policydenypublisher allowfinaldraft
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositorysid.inpe.br/mtc-m19@80/2009/08.21.17.02.53
Next Higher Units8JMKD3MGPCW/446AF4B
DisseminationWEBSCI; PORTALCAPES; COMPENDEX.
Host Collectionsid.inpe.br/mtc-m19@80/2009/08.21.17.02
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress electronicmailaddress format isbn keywords label lineage mark month nextedition notes number orcid pages parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url
7. Description control
e-Mail (login)marciana
update 


Close