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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m16.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Repositorysid.inpe.br/marciana/2004/01.29.12.39
Last Update2009:03.11.18.07.26 (UTC) administrator
Metadata Repositorysid.inpe.br/marciana/2004/01.29.12.39.40
Metadata Last Update2018:06.05.01.20.51 (UTC) administrator
Secondary KeyINPE-10385-PRE/5885
Citation KeyMarquesCost:2003:PuPlTh
TitlePulsed plasma thruster development
FormatOn-line
Year2003
Access Date2024, May 15
Secondary TypePRE CI
Number of Files1
Size1264 KiB
2. Context
Author1 Marques, Rodrigo Intini
2 Costa, Fernando de Souza
Resume Identifier1
2 8JMKD3MGP5W/3C9JH46
Group1 LCP-INPE-MCT-BR
Affiliation1 Laboratório Associado de Combustão e Propulsão, INPE
Conference NameInternaitonal Congress of Mathematical Engeneering, 17.
Conference LocationSão Paulo
Date10-14 nov. 2003
PublisherABCM
Publisher CitySao Paulo
Book TitleAnais
Tertiary TypePapers
History (UTC)2008-06-10 23:03:29 :: administrator -> marciana ::
2009-03-11 18:07:26 :: marciana -> administrator ::
2018-06-05 01:20:51 :: administrator -> marciana :: 2003
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Keywordsadvanced propulsion
plasma thruster
PPT
satellite
space probe
AbstractThis work describes the preliminary design and the initial development of a pulsed plasma thruster (PPT) to test different fuels, geometries, energies of discharge, voltages and frequencies. A PPT is an electric thruster used for attitude control and orbit correction of satellites and space probes. It uses a high-voltage discharge applied to the surface of a solid propellant bar. The propellant is ablated, ionized and accelerated by a combination of electromagnetic forces (Lorenz Force) and thermal expansion to create usable thrust. The PPT comprises a control circuit, a direct current converter (DC-DC) and a discharge chamber. The discharge chamber chosen includes a solid annular Teflon rod as fuel and two concentric cylindrical electrodes of copper. Three PPT versions were developed. The first version used an 8µF capacitor charged with 24 V yielding 2.304 mJ per pulse with a 10 kV discharge. The second version had an 4 µF capacitor loaded with 169.7 V yielding 57.6 mJ per pulse with a 18 kV discharge. It was tested in a vacuum chamber for 7.5 hours, generating 1,616,400 pulses at 60 Hz with total mass variation of 45.1 mg, with 0.028 µg ablated per pulse and a calculated impulse bit of 1.12 µNs. The third version under development allows operation at different frequencies 0.1-10 Hz, pulse energies 0.1-10 J and discharge voltages 10-40 kV. This version will permit the validation of thruster components for use on different missions.
AreaCOMB
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABCP > Pulsed plasma thruster...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
data URLhttp://urlib.net/ibi/sid.inpe.br/marciana/2004/01.29.12.39
zipped data URLhttp://urlib.net/zip/sid.inpe.br/marciana/2004/01.29.12.39
Languageen
Target Filepulsed.pdf
User Groupadministrator
marciana
Visibilityshown
Copy HolderSID/SCD
Read Permissionallow from all
5. Allied materials
Next Higher Units8JMKD3MGPCW/3ET38CH
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.46.07 1
Host Collectionsid.inpe.br/banon/2003/08.15.17.40
6. Notes
Empty Fieldsarchivingpolicy archivist callnumber copyright creatorhistory descriptionlevel dissemination documentstage doi e-mailaddress edition editor electronicmailaddress identifier isbn issn label lineage mark mirrorrepository nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark type url versiontype volume
7. Description control
e-Mail (login)marciana
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