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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21c.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34R/3SMPRQ2
Repositorysid.inpe.br/mtc-m21c/2019/02.07.16.39   (restricted access)
Last Update2019:02.07.16.39.24 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21c/2019/02.07.16.39.24
Metadata Last Update2019:04.29.03.23.49 (UTC) administrator
DOI10.1615/IntJEnergeticMaterialsChemProp.2018029025
ISSN2150-7678
Citation KeyMaschioPerMeyMarVie:2018:DoStHy
TitleA doe study on the hypergolicity of hydrogen peroxide with a rocket liquid fuel based on monoethanolamine and ethanol
Year2018
Access Date2024, May 06
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size626 KiB
2. Context
Author1 Maschio, Leandro José
2 Pereira, Luis Gustavo Ferroni
3 Meyer, Willian Müller
4 Marques, Rodrigo Intini
5 Vieira, Ricardo
Resume Identifier1
2
3
4
5 8JMKD3MGP5W/3C9JJ68
Group1 PCP-ETES-SESPG-INPE-MCTIC-GOV-BR
2
3 PCP-ETES-SESPG-INPE-MCTIC-GOV-BR
4 LABCP-COCTE-INPE-MCTIC-GOV-BR
5 LABCP-COCTE-INPE-MCTIC-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Universidade Federal de Lavras (UFLA)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
4 Instituto Nacional de Pesquisas Espaciais (INPE)
5 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1
2
3
4 rodrigo.intini@inpe.br
5 ricardo.vieira@inpe.br
JournalInternational Journal of Energetic Materials and Chemical Propulsion
Volume17
Number2
Pages137-145
History (UTC)2019-02-07 16:40:00 :: simone -> administrator :: 2018
2019-04-29 03:23:49 :: administrator -> simone :: 2018
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
Keywordsignition delay
liquid propulsion
hypergolic
green propellants
monoethanolamine
ethanol
AbstractIn the last decades there has been an increasing interest in low-cost, low environmental impact liquid propulsion systems, while safety and a short development cycle continue to be essential requirements. This work presents the development of an ethanol and monoethanolamine based rocket fuel, hypergolic with hydrogen peroxide (H2O2), featuring low toxicity and high density-specific-impulse. Initially, a set of tests was carried out to evaluate this parameter in a range of compositions prepared with several catalysts dissolved in monoethanolamine. Among the catalytic materials tested, copper nitrate revealed the shortest ignition delay. Subsequently, a Design of Experiments approach was applied to select the ethanol and catalyst content in the fuel capable of decreasing the ignition delay of the reaction. The results showed that an optimized fuel composition with 61% monoethanolamine, 30% ethanol, and 9% hydrated copper nitrate weight percent, yielded a minimum ignition delay of 15.7 ms.
AreaCOMB
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4. Conditions of access and use
Languageen
Target Filemachio_doe.pdf
User Groupsimone
Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryurlib.net/www/2017/11.22.19.04.03
Next Higher Units8JMKD3MGPCW/3ET38CH
8JMKD3MGPCW/3F35D8B
DisseminationWEBSCI; PORTALCAPES; SCOPUS.
Host Collectionurlib.net/www/2017/11.22.19.04
6. Notes
Empty Fieldsalternatejournal archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark month nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype url
7. Description control
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