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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21c.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34R/4497CA2
Repositorysid.inpe.br/mtc-m21c/2021/03.01.12.00   (restricted access)
Last Update2021:03.01.12.00.59 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21c/2021/03.01.12.00.59
Metadata Last Update2022:04.03.23.14.26 (UTC) administrator
DOI10.1615/IntJEnergeticMaterialsChemProp.2020032684
ISSN2150-7678
Citation KeyMaschioAraPerGouVie:2021:AsPeGr
TitleAssessing the performance of a green liquid fuel hypergolic with hydrogen peroxide in a 50 n bipropellant thruster
Year2021
Access Date2024, May 19
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size3364 KiB
2. Context
Author1 Maschio, Leandro José
2 Araújo, Emmanuel Péres de
3 Pereira, Luís Gustavo Ferroni
4 Gouvêa, Leonardo Henrique
5 Vieira, Ricardo
Resume Identifier1
2
3
4
5 8JMKD3MGP5W/3C9JJ68
Group1 PCP-ETES-DIPGR-INPE-MCTI-GOV-BR
2
3
4
5 COPDT-CGIP-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Universidade de São Paulo (USP)
3 Instituto Tecnológico de Aeronáutica (ITA)
4 Instituto Tecnológico de Aeronáutica (ITA)
5 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 ljmaschio@gmail.com
2
3
4
5 ricardo.vieira@inpe.br
JournalInternational Journal of Energetic Materials and Chemical Propulsion
Volume20
Number1
Pages21-30
History (UTC)2021-03-01 12:02:26 :: simone -> administrator :: 2021
2022-04-03 23:14:26 :: administrator -> simone :: 2021
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
Keywordshydrogen peroxide
liquid propulsion
hypergolic
green propellants
monoethanolamine
ethanol
AbstractThe last decades have witnessed an increasing interest in the development of green propellants for propulsion systems. Particularly in the low thrust domain, where a feasible alternative to the storable liquid bipropellant system hydrazine nitrogen tetroxide is yet to be fully demonstrated, the application of green hypergolic propellants such as ethanol and H2O2 90 wt% appears to be a promising one. This work presents the design and firing test of a 50 N bipropellant thruster based on the H2O2 90 wt% monoethanolamine-ethanol hypergolic pair catalyzed by Cu2+, previously developed by our research group. The 5 s firing test, conducted under a swirl injection scheme, yielded average values of 50.38 N, 147 s, and 1210 m/s for thrust, Isp, and c*, respectively, with the target value of 5 bar for the chamber pressure being reached after 2 s of operation. Alongside with a c* efficiency of 84%, these results suggest that the assessed green hypergolic bipropellant pair may be a promising alternative for applications in the low-thrust range.
AreaCOMB
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4. Conditions of access and use
Languageen
Target Filemaschio_assessing.pdf
User Groupsimone
Reader Groupadministrator
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Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/3F35D8B
8JMKD3MGPCW/46KUES5
Citing Item Listsid.inpe.br/bibdigital/2022/04.03.23.11 4
sid.inpe.br/mtc-m21/2012/07.13.14.59.12 2
sid.inpe.br/bibdigital/2013/10.14.22.36 1
DisseminationWEBSCI; PORTALCAPES; SCOPUS.
Host Collectionurlib.net/www/2017/11.22.19.04
6. Notes
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