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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m16b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Repositorysid.inpe.br/mtc-m17@80/2007/09.04.18.50
Last Update2007:09.04.18.50.28 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m17@80/2007/09.04.18.50.30
Metadata Last Update2018:06.05.03.34.46 (UTC) administrator
Citation KeyMarquesGabrCost:2007:PrReHi
TitlePreliminary results of a high frequency pulsed fronts inside wood rockets
Year2007
Access Date2024, May 15
Secondary TypePRE CI
Number of Files1
Size471 KiB
2. Context
Author1 Marques, R. I.
2 Gabriel, s. B.
3 Costa, Fernando de Souza
Resume Identifier1
2
3 8JMKD3MGP5W/3C9JH46
Group1
2
3 LCP-INPE-MCT-BR
Affiliation1 University of Southampton
2 University of Southampton
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Conference NameAIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 43.
Conference LocationCincinati, OH
Date8-11 july
Book TitleProceedings
Tertiary TypePaper
OrganizationAIAA
History (UTC)2007-09-04 19:13:24 :: ignes@lcp.inpe.br -> administrator ::
2012-10-23 23:57:10 :: administrator -> ignes@lcp.inpe.br :: 2007
2013-02-20 16:41:05 :: ignes@lcp.inpe.br -> administrator :: 2007
2018-06-05 03:34:46 :: administrator -> marciana :: 2007
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
AbstractABSTRACT: - Pulsed Plasma Thrusters (PPTs) are long standing electric propulsion thrusters that are reliable, relatively simple and low cost. One of the main issues with PPTs is its low efficiency (discharge energy vs. exhaust jet‟s kinetic energy), typically between 3-8%. One of the main contributors for the low performance in PPTs is the late time ablation (LTA). LTA is the sublimation of propellant that takes place after the main discharge, due to the propellant, usually Teflon®, temperature being above its sublimation point. The LTA produces a low speed gas and macro particles that does not contribute significantly to produce thrust. The High Frequency Pulsed Plasma Thruster (HFB-PPT) is a novel patented design that aims at accelerating the late time ablation by employing additional discharges after the main discharge. This paper presents the HFB-PPT concept and preliminary results.
AreaCOMB
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABCP > Preliminary results of...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
data URLhttp://mtc-m16b.sid.inpe.br/ibi/sid.inpe.br/mtc-m17@80/2007/09.04.18.50
zipped data URLhttp://mtc-m16b.sid.inpe.br/zip/sid.inpe.br/mtc-m17@80/2007/09.04.18.50
Languageen
Target Filepreliminary.pdf
User Groupadministrator
ignes@lcp.inpe.br
Visibilityshown
5. Allied materials
Next Higher Units8JMKD3MGPCW/3ET38CH
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.46.07 1
Host Collectionlcp.inpe.br/ignes/2004/02.12.18.39
cptec.inpe.br/walmeida/2003/04.25.17.12
6. Notes
Empty Fieldsarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination documentstage doi e-mailaddress edition editor electronicmailaddress format identifier isbn issn keywords label lineage mark mirrorrepository nextedition notes numberofvolumes orcid pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress readergroup readpermission rightsholder schedulinginformation secondarydate secondarykey secondarymark serieseditor session shorttitle sponsor subject tertiarymark type url versiontype volume
7. Description control
e-Mail (login)marciana
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