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1. Identificação
Tipo de ReferênciaArtigo em Revista Científica (Journal Article)
Sitemtc-m21d.sid.inpe.br
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identificador8JMKD3MGP3W34T/45NC5BP
Repositóriosid.inpe.br/mtc-m21d/2021/11.03.14.50   (acesso restrito)
Última Atualização2021:11.03.14.50.14 (UTC) simone
Repositório de Metadadossid.inpe.br/mtc-m21d/2021/11.03.14.50.14
Última Atualização dos Metadados2022:04.03.23.14.05 (UTC) administrator
DOI10.1088/1361-6501/ac271d
ISSN0957-0233
1361-6501
Chave de CitaçãoSoaresMarq:2021:VaDySt
TítuloIn vacuum dynamic and static tests of a thrust balance for electric propulsion with hysteresis analysis and behaviour prediction with transfer function
Ano2021
MêsDec.
Data de Acesso20 maio 2024
Tipo de Trabalhojournal article
Tipo SecundárioPRE PI
Número de Arquivos1
Tamanho3876 KiB
2. Contextualização
Autor1 Soares, Diogo Leon Oliveira
2 Marques, Rodrigo Intini
ORCID1 0000-0003-1859-3900
2 0000-0001-6940-3578
Grupo1 PCP-ETES-DIPGR-INPE-MCTI-GOV-BR
2 COPDT-CGIP-INPE-MCTI-GOV-BR
Afiliação1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Endereço de e-Mail do Autor1 diogo.leon@inpe.br
2 rodrigo.intini@inpe.br
RevistaMeasurements Science and Technology
Volume32
Número12
Páginase125903
Histórico (UTC)2021-11-03 14:50:21 :: simone -> administrator :: 2021
2022-04-03 23:14:05 :: administrator -> simone :: 2021
3. Conteúdo e estrutura
É a matriz ou uma cópia?é a matriz
Estágio do Conteúdoconcluido
Transferível1
Tipo do ConteúdoExternal Contribution
Tipo de Versãopublisher
Palavras-Chaveelectric propulsion
hystersis
magnetic damper
thrust measurement
torsinal thrust balance
transfer function
two-stage pulsed plasma thruster
ResumoThis work describes the advances on the development of a thrust-stand for electric propulsion application with a focus on the constraints of the two-stage pulsed plasma thruster (TS-PPT) being developed at INPE at the Electric Propulsion Laboratory (LPEL) of the Laboratory of Combustion and Propulsion (LABCP). While previous work on this instrument focused on basic development in atmospheric pressure the present effort presents the development undertaken to elevate the TRL of the device to allow it to operate in vacuum - the environment where actual electric thrusters operate and are tested. To cater for INPE's TS-PPT specification, standard masses summing 1.2 kg were used while the electrostatic calibration device (ECD) was set to produce 31 μNs. A detailed hysteresis analysis was carried out at the target TS-PPT specification together with a transfer function that aimed at extrapolating and predicting the behaviour of the instrument. In addition, this work shows the development of a new magnetic damper for the instrument that reduces the waiting time between tests. A new calibration at the TS-PPT specification points were undertaken in vacuum since previous calibration were made for atmospheric pressure and did not include the specific points of interest for the TS-PPT. Furthermore, previous calibration procedures were verified to ensure they would apply to the vacuum conditions and to account for the substitution of some thrust stand previously incompatible vacuum parts and also to account for the addition of the new magnetic damper and other unforeseen conditions caused by the vacuum environment.
ÁreaCOMB
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4. Condições de acesso e uso
Idiomaen
Arquivo Alvosoares_vacuum.pdf
Grupo de Usuáriossimone
Grupo de Leitoresadministrator
simone
Visibilidadeshown
Política de Arquivamentodenypublisher denyfinaldraft12
Permissão de Leituradeny from all and allow from 150.163
Permissão de Atualizaçãonão transferida
5. Fontes relacionadas
Unidades Imediatamente Superiores8JMKD3MGPCW/3F35D8B
8JMKD3MGPCW/46KUES5
Lista de Itens Citandosid.inpe.br/bibdigital/2022/04.03.23.11 7
sid.inpe.br/bibdigital/2013/10.14.22.36 2
DivulgaçãoSCOPUS
Acervo Hospedeirourlib.net/www/2021/06.04.03.40
6. Notas
Campos Vaziosalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark mirrorrepository nextedition notes parameterlist parentrepositories previousedition previouslowerunit progress project resumeid rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype url
7. Controle da descrição
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