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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP5W34M/3FA45TQ
Repositorysid.inpe.br/mtc-m21b/2013/11.26.17.00.58   (restricted access)
Last Update2017:07.21.18.25.39 (UTC) marcelo.pazos@inpe.br
Metadata Repositorysid.inpe.br/mtc-m21b/2013/11.26.17.00.59
Metadata Last Update2021:02.11.18.12.13 (UTC) administrator
DOI10.4028/www.scientific.net/AMM.319.427
ISBN9783037856864
ISSN1660-9336
Labelscopus 2013-11
Citation KeyVasquesSouz:2013:InLoPr
TitleInvestigation of the Lox/Alcohol propulsion system
Year2013
Access Date2024, May 19
Secondary TypePRE PI
Number of Files1
Size405 KiB
2. Context
Author1 Vasques, Bruno Barreto
2 Souza, Luiz Carlos Gadelha de
Resume Identifier1
2 8JMKD3MGP5W/3C9JHN3
Group1
2 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1
2 gadelha@dem.inpe.br
e-Mail Addressmarcelo.pazos@inpe.br
JournalApplied Mechanics and Materials
Volume319
Pages427-432
Secondary MarkB2 B3 B3
History (UTC)2016-07-03 20:59:12 :: administrator -> marcelo.pazos@inpe.br :: 2013
2017-07-21 18:25:39 :: marcelo.pazos@inpe.br -> administrator :: 2013
2021-02-11 18:12:13 :: administrator -> marcelo.pazos@inpe.br :: 2013
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
Keywordsgreen propellants
liquid propellant rocket engine
liquid propulsion
regenerative cooling
second generation
space transportation system
system development
technology advancement
finite element method
propulsion
rocket engines
propellants
AbstractThis work describes the design of a liquid propellant rocket engine using non-toxic, low-cost propellants, for a second generation space transportation system. The primary goals of this effort were to identify the most attractive fuel and system design approach for sizing a workhorse engine and to determine technology advancements that are needed to provide subsequent system development. The emphasis of the analysis was directed toward propellant perfomance and engine characterization. On the basis of operational and cost criteria, ethanol was determined to be the best fuel candidate. Because of the high heat flux conditions at high chamber pressures, regenerative cooling was chosen as the preferred method of wall protection, leaving film cooling as a supplementary chamber cooling method. A finite element analysis was carried out to evaluate thrust chamber reliability on steady working operation and hydraulic test mode. The study contributed to establish a better understanding of propellant potentialities and to investigate the best means of utilizing these capabilities in typical engine designs. © (2013) Trans Tech Publications, Switzerland.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Investigation of the...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
User Groupadministrator
marcelo.pazos@inpe.br
Reader Groupadministrator
marcelo.pazos@inpe.br
Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryiconet.com.br/banon/2006/11.26.21.31
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.54.10 4
sid.inpe.br/bibdigital/2021/02.11.18.06 3
DisseminationWEBSCI; COMPENDEX; SCOPUS.
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
Empty Fieldsalternatejournal archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel format lineage mark month nextedition notes number orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject targetfile tertiarymark tertiarytype typeofwork url
7. Description control
e-Mail (login)marcelo.pazos@inpe.br
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