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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34P/3HJTRU8
Repositorysid.inpe.br/mtc-m21b/2014/12.18.11.25
Last Update2014:12.18.11.25.12 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21b/2014/12.18.11.25.12
Metadata Last Update2018:06.04.03.04.41 (UTC) administrator
Secondary KeyINPE--PRE/
Citation KeyMarinMarq:2014:PeAnDo
TitlePerformance analysis of a double discharge pulsed plasma thruster by varying the energy of its two stages
Year2014
Access Date2024, Apr. 26
Secondary TypePRE CI
Number of Files1
Size822 KiB
2. Context
Author1 Marin, Luis Francisco Chrispim
2 Marques, Rodrigo Intini
Group1 PCP-ETES-SPG-INPE-MCTI-GOV-BR
2 LCP-CTE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
e-Mail Addressmarcelo.pazos@inpe.br
Conference NameLatin American IAA CubeSat Workshop, 1.
Conference LocationBrasília
Date8-11 dez., 2014
Tertiary TypeOral Technical Session
History (UTC)2014-12-18 11:25:12 :: marcelo.pazos@sid.inpe.br -> administrator ::
2018-06-04 03:04:41 :: administrator -> marcelo.pazos@inpe.br :: 2014
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
AbstractA Pulsed Plasma Thruster (PPT) is an electric space propulsion device mostly used for spacecraft orbit maintenance and attitude control. One of the most common issues with PPTs is the Late Time Ablation (LTA) - the sublimation of propellant that occurs after the main electric discharge, reducing propellant use efficiency. The Double Discharge PPT (DD-PPT) has two stages: The first stage works as a regular PPT and the second stage employs additional electric discharges to accelerate the first dis-charge plasma and the LTA. This work studied a DD-PPT and analyzed its efficiency and performance while varying the levels of energy employed on each of the two stages in order to archive maximum performance. A new electric circuit was designed to enable energy levels distribution amongst the two stages of the DD-PPT. An oscilloscope and a Rogowski current probe were used to estimate the impulse bit and a precision scale was used for measuring propellant mass variation. Inductance gradients were calculated using a mathematical model. Thruster tests were performed in a vacuum chamber with pres-sure of ~10-6 mbar. The results showed a significant increase in specific impulse. The optimum config-uration of energy distribution occurred when a smaller percentage of the total energy was employed in the primary stage (for ablation) and a greater percentage of the total energy was employed in the second stage, used for plasma acceleration.
AreaCOMB
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4. Conditions of access and use
data URLhttp://urlib.net/ibi/8JMKD3MGP3W34P/3HJTRU8
zipped data URLhttp://urlib.net/zip/8JMKD3MGP3W34P/3HJTRU8
Languageen
Target FileWorkshop_Brasilia_artigo_v20_English_FINAL.pdf
User Groupmarcelo.pazos@inpe.br
Reader Groupadministrator
marcelo.pazos@inpe.br
Visibilityshown
Read Permissionallow from all
Update Permissionnot transferred
5. Allied materials
Mirror Repositorysid.inpe.br/mtc-m21b/2013/09.26.14.25.22
Next Higher Units8JMKD3MGPCW/3ET38CH
8JMKD3MGPCW/3F35D8B
Citing Item Listsid.inpe.br/bibdigital@80/2006/04.07.15.50.13 2
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
Empty Fieldsarchivingpolicy archivist booktitle callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi edition editor electronicmailaddress format isbn issn keywords label lineage mark nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress resumeid rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark type url versiontype volume
7. Description control
e-Mail (login)marcelo.pazos@inpe.br
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