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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21c.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34R/436PA5H
Repositorysid.inpe.br/mtc-m21c/2020/09.01.14.22   (restricted access)
Last Update2020:09.01.14.22.24 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21c/2020/09.01.14.22.25
Metadata Last Update2022:01.04.01.35.19 (UTC) administrator
DOI10.1002/prep.202000020
ISSN0721-3115
Citation KeyPereiraMasAraGouVie:2020:CoOxSu
TitleCoMn-spinel oxides as supported catalyst for rocket-grade hydrogen peroxide decomposition
Year2020
Access Date2024, May 19
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size1548 KiB
2. Context
Author1 Pereira, Luís Gustavo Ferroni
2 Maschio, Leandro José
3 Araújo, Emmanuel Péres de
4 Gouvêa, Leonardo Henrique
5 Vieira, Ricardo
Resume Identifier1
2
3
4
5 8JMKD3MGP5W/3C9JJ68
Group1
2 PCP-ETES-SESPG-INPE-MCTIC-GOV-BR
3
4
5 LABCP-COCTE-INPE-MCTIC-GOV-BR
Affiliation1 Instituto Tecnológico de Aeronáutica (ITA)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Universidade de São Paulo (USP)
4 Instituto Tecnológico de Aeronáutica (ITA)
5 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1
2
3
4
5 ricardo.vieira@inpe.br
JournalPropellants, Explosives, Pyrotechnics
Volume45
Pages1-8
History (UTC)2020-09-01 14:23:01 :: simone -> administrator :: 2020
2022-01-04 01:35:19 :: administrator -> simone :: 2020
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsSpinels
Monopropellants
Catalysts
Hydrogen peroxide
Green propellants
AbstractThis work presents the application of a cobalt and manganese mixed oxides-based catalyst with spinel structure to the decomposition of the storable green monopropellant H(2)O(2)90 wt%. The 5.4 % Co0.5Mn2.5O4/Al(2)O(3)catalyst was tested in a series of continuous and pulsed 2 N thruster firings, yielding a fast and repetitive performance, spontaneously and completely decomposing H(2)O(2)90 wt% without undergoing deactivation or fragmentation during the tests. A specific impulse of 104 s and a characteristic velocity of 881 m/s were reached, so that the characteristic velocity efficiency amounted to 93.7 %. The adiabatic decomposition temperature of the monopropellant (756 degrees C) was also reached, thus evidencing the effectiveness of the 5.4 % Co0.5Mn2.5O4/Al(2)O(3)catalyst. Its excellent activity in the decomposition of H(2)O(2)90 wt% was attributed to the presence of the redox pairs Mn2+/Mn(3+)and Co2+/Co3+, therefore making it a feasible material for low and medium thrust propulsive systems.
AreaCOMB
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4. Conditions of access and use
Languageen
Target Filepereira_comn.pdf
User Groupsimone
Reader Groupadministrator
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Visibilityshown
Archiving Policydenypublisher denyfinaldraft
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/3ET38CH
8JMKD3MGPCW/3F35D8B
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.59.12 3
sid.inpe.br/bibdigital/2013/10.14.22.36 1
DisseminationWEBSCI; PORTALCAPES; 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 number orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype url
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