Close
Metadata

1. Identity statement
Reference TypeJournal Article
Sitemtc-m21c.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34R/3RPEDQ2
Repositorysid.inpe.br/mtc-m21c/2018/09.04.18.27
Last Update2018:09.04.18.27.09 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21c/2018/09.04.18.27.09
Metadata Last Update2021:02.11.18.10.44 (UTC) administrator
DOI10.5028/jatm.v10.914
ISSN1984-9648
Citation KeyMotaHincRoccSchl:2018:MoAnLO
TitleModeling and analysis of a LOX/ethanol liquid rocket engine
Year2018
Access Date2024, May 16
Type of Workjournal article
Secondary TypePRE PN
Number of Files1
Size1430 KiB
2. Context
Author1 Mota, F. A. S.
2 Hinckel, J. N.
3 Rocco, Evandro Marconi
4 Schlingloff, H.
Resume Identifier1
2
3 8JMKD3MGP5W/3C9JH37
ORCID1 0000-0003-3672-0547
2 0000-0002-0171-2697
3 0000-0003-0660-0587
4 0000-0003-1806-9113
Group1
2
3 DIDMC-CGETE-INPE-MCTIC-GOV-BR
Affiliation1
2
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1
2
3 evandro_mr@yahoo.com.br
JournalJournal of Aerospace Technology and Management
Volume10
Numbere3018
Secondary MarkB2_PLANEJAMENTO_URBANO_E_REGIONAL_/_DEMOGRAFIA B3_INTERDISCIPLINAR B4_GEOCIÊNCIAS B4_ENGENHARIAS_II B4_CIÊNCIAS_AMBIENTAIS B5_ENGENHARIAS_IV B5_ENGENHARIAS_III B5_CIÊNCIA_DA_COMPUTAÇÃO C_ASTRONOMIA_/_FÍSICA
History (UTC)2018-09-04 18:27:09 :: simone -> administrator ::
2018-09-04 18:27:09 :: administrator -> simone :: 2018
2018-09-04 18:27:23 :: simone -> administrator :: 2018
2021-02-11 18:10:44 :: administrator -> simone :: 2018
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsLiquid rocket engines
Ethanol
Modeling
AbstractThis work studies the performance and dry mass of the under development LOX/Ethanol L75 liquid rocket engine. To this end, an object-oriented program written in C++ was developed. The program is intended to be versatile and easily extensible in order to analyze different configurations of liquid rocket engines. The UML (Unified Modeling Language) tool is used to model the architecture of the codes. UML diagrams help to visualize the code structure and the communication between objects, enabling a high degree of abstraction. The cryogenics Vulcain and HM7B engines power cycles along with the staged-combustion SSME engine perform the verification of the codes. Finally, the influence of changes in design parameters on the performance and dry mass of the L75 rocket engine is analyzed.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Modeling and analysis...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Content
agreement.html 04/09/2018 15:27 1.0 KiB 
4. Conditions of access and use
data URLhttp://urlib.net/ibi/8JMKD3MGP3W34R/3RPEDQ2
zipped data URLhttp://urlib.net/zip/8JMKD3MGP3W34R/3RPEDQ2
Languageen
Target Filemota_modeling.pdf
User Groupsimone
Reader Groupadministrator
simone
Visibilityshown
Archiving Policyallowpublisher allowfinaldraft
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.45.41 6
sid.inpe.br/bibdigital/2021/02.11.18.06 4
DisseminationWEBSCI; PORTALCAPES; COMPENDEX; SCOPUS.
Host Collectionurlib.net/www/2017/11.22.19.04
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark mirrorrepository month nextedition notes pages parameterlist parentrepositories previousedition previouslowerunit progress project readpermission rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url
7. Description control
e-Mail (login)simone
update 


Close