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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m16.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Repositorysid.inpe.br/marciana/2004/01.28.15.52
Last Update2009:03.11.18.14.55 (UTC) administrator
Metadata Repositorysid.inpe.br/marciana/2004/01.28.15.52.10
Metadata Last Update2021:02.11.18.15.09 (UTC) administrator
Secondary KeyINPE-10387-PRE/5887
Citation KeySallesSeHiBoCaBa:2003:Re20Fu
TitleResurges in 200N fuel film cooling bipropellant engine
FormatOn-line
ProjectMotores a Bipropelentes Líquidos
Year2003
Access Date2024, May 15
Secondary TypePRE CI
Number of Files1
Size336 KiB
2. Context
Author1 Salles, Carlos Eduardo Rolfsen
2 Serra Jr., Aguinaldo Martins
3 Hinckel, José Nivaldo
4 Botura Jr., Galdenoro
5 Carvalho Jr., João Andrade de
6 Bastos Netto, Demétrio
Resume Identifier1 8JMKD3MGP5W/3C9JGQP
2
3 8JMKD3MGP5W/3C9JHHU
4
5
6 8JMKD3MGP5W/3C9JGTG
Group1 LCP-INPE-MCT-BR
2
3 DMC-INPE-MCT-BR
4
5 LCP-INPE-MCT-BR
6 LCP-INPE-MCT-BR
Affiliation1 Combustão, Instituto Nacional de Pesquisas Espaciais. Laboratório de
2 Guaratinguetá, Universidade Estadual Paulista. faculdade de Engenharia de
Conference NameSpace Generation Congress: Building an active global community.
Conference LocationBremen, Germany
Date26-28, Sep. 2003
PublisherDLR
Book TitleProceedings
History (UTC)2006-11-09 18:34:50 :: administrator -> marciana ::
2007-03-14 18:02:37 :: marciana -> administrator ::
2008-06-10 23:03:28 :: administrator -> marciana ::
2009-03-11 18:14:55 :: marciana -> administrator ::
2021-02-11 18:15:09 :: administrator -> marciana :: 2003
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
KeywordsPROPULSÃO
bipropellant engine
AbstractA 200N bipropellant engine under development was tested in the Test Bench with Altitude Simulation located at the National Institute for Space Research, Cachoeira Paulista, Brazil. During the firings very high amplitude pressure oscillations in the combustion chamber were observed. Pressure oscillations more than 40% of the chamber mean pressure imposed very high heat transfer rates to the wall, throat nozzle and injector face, leading to the overall engine failure. This work discusses the onset of the above behavior and relates it with the Resurge effect phenomenon described earlier during the development of the much larger F-1 Rocket Engine.
AreaCOMB
Arrangement 1urlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABCP > Resurges in 200N...
Arrangement 2urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Resurges in 200N...
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/sid.inpe.br/marciana/2004/01.28.15.52
zipped data URLhttp://urlib.net/zip/sid.inpe.br/marciana/2004/01.28.15.52
Languageen
Target Fileresurges.pdf
User Groupadministrator
marciana
Visibilityshown
Copy HolderSID/SCD
Read Permissionallow from all
5. Allied materials
Next Higher Units8JMKD3MGPCW/3ET38CH
8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.44.29 3
Host Collectionsid.inpe.br/banon/2003/08.15.17.40
6. Notes
Empty Fieldsarchivingpolicy archivist callnumber copyright creatorhistory descriptionlevel dissemination documentstage doi e-mailaddress edition editor electronicmailaddress identifier isbn issn label lineage mark mirrorrepository nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress publisheraddress readergroup rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url versiontype volume
7. Description control
e-Mail (login)marciana
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