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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
IdentifierJ8LNKAN8RW/38MR2T8
Repositorydpi.inpe.br/plutao/2010/12.02.14.25
Last Update2011:02.23.18.30.01 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao/2010/12.02.14.25.54
Metadata Last Update2018:06.05.00.12.32 (UTC) administrator
Secondary KeyINPE--PRE/
ISSN1678-5878
Labellattes: 6600426630222951 1 CostaViei:2010:PrAnHy
Citation KeyCostaViei:2010:PrAnHy
TitlePreliminary Analysis of Hybrid Propulsion Systems for Launching Nanosats
Year2010
Access Date2024, May 15
Secondary TypePRE PI
Number of Files1
Size255 KiB
2. Context
Author1 Costa, Fernando de Souza
2 Vieira, Ricardo
Resume Identifier1 8JMKD3MGP5W/3C9JH46
2 8JMKD3MGP5W/3C9JJ68
Group1 LCP-CTE-INPE-MCT-BR
2 LCP-CTE-INPE-MCT-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 fernando@lcp.inpe.br
e-Mail Addressfernando@lcp.inpe.br
JournalJournal of the Brazilian Society of Mechanical Sciences and Engineering
Volume32
Number4
Pages1-9
Secondary MarkB2_ARQUITETURA_E_URBANISMO C_ASTRONOMIA_/_FÍSICA B4_CIÊNCIA_DA_COMPUTAÇÃO B4_CIÊNCIAS_BIOLÓGICAS_I B2_ENGENHARIAS_I B2_ENGENHARIAS_II B2_ENGENHARIAS_III B4_ENGENHARIAS_IV B1_INTERDISCIPLINAR B5_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA B2_MATERIAIS B3_ODONTOLOGIA B3_SAÚDE_COLETIVA
History (UTC)2010-12-06 14:15:32 :: lattes -> ricardo :: 2010
2010-12-07 11:40:46 :: ricardo -> marciana :: 2010
2011-02-23 18:30:01 :: marciana -> administrator :: 2010
2011-06-04 15:44:57 :: administrator -> marciana :: 2010
2011-09-20 14:13:31 :: marciana -> administrator :: 2010
2018-06-05 00:12:32 :: administrator -> marciana :: 2010
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsPropulsão híbrida
Parafina
H2O2
Análise de missão
hybrid rocket
paraffin
H2O2
nanosats
low Earth orbit (LEO)
AbstractThis work determines the preliminary mass distribution of hybrid rockets using 98% H2O2 and solid paraffin mixed with aluminum as propellants. An iterative process is used to calculate the rocket performance characteristics and to determine the inert mass fraction from given initial conditions. It is considered a mission to place a 20 kg payload into a 300 km circular equatorial orbit by air launched and ground launched hybrid rockets using three stages. The results indicate total initial masses of about 7800 kg for a ground launched hybrid rocket and 4700 kg for an air launched hybrid rocket.
AreaCOMB
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABCP > Preliminary Analysis of...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
data URLhttp://urlib.net/ibi/J8LNKAN8RW/38MR2T8
zipped data URLhttp://urlib.net/zip/J8LNKAN8RW/38MR2T8
Languagept
Target Filev32n4a12.pdf
User Groupadministrator
lattes
marciana
Visibilityshown
Archiving Policyallowpublisher allowfinaldraft
Read Permissionallow from all
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/3ET38CH
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.46.07 4
sid.inpe.br/bibdigital@80/2006/04.07.15.50.13 1
DisseminationPORTALCAPES
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
NotesSetores de Atividade: Administração Pública, Defesa e Seguridade Social.
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel doi format isbn lineage mark mirrorrepository month nextedition orcid 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
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