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4 referências encontradas buscando em 15 dentre 15 sites.
Data e hora local de busca: 19/10/2020 12:34.
Tipo da ReferênciaConference Proceedings
Identificador8JMKD3MGP3W34P/3L9KRKP
Repositóriosid.inpe.br/mtc-m21b/2016/03.03.12.26
Metadadossid.inpe.br/mtc-m21b/2016/03.03.12.26.21
Sitemtc-m21b.sid.inpe.br
Chave SecundáriaINPE--PRE/
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Chave de CitaçãoMahlmeisterRoPaFeAuFiMa:2016:PeMo
Autor1 Mahlmeister, Felipe Lima
2 Romano, Rodrigo Alvite
3 Parro, Vanderlei Cunha
4 Ferrão, Rafael Corsi
5 Augusto, Sérgio Ribeiro
6 Finco, Saulo
7 Manea, Silvio
Grupo1
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3
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5
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7 SGP-ETE-INPE-MCTI-GOV-BR
Afiliação1
2
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7 Instituto Nacional de Pesquisas Espaciais (INPE)
Endereço de e-Mail do Autor1
2
3
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5
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7 silvio.manea@inpe.br
TítuloCUBESAT frame design - peta model
Nome do EventoLatin American IAA CubeSat Workshop, 2
Ano2016
Data28 Feb. - 02 Mar.
Localização do EventoFlorianópolis, SC
ResumoThis summary deals with the development of a modular structure with conceptual focus on the disposal of PCBs (printed circuit board) in a CubeSat, where instead of the traditional format in which the cards are stacked inside, the electronic boards are positioned in the hub side in order to achieve greater internal space for payloads, as well as facilitating the access of PCBs during assembly and testing. This concept was titled as "petal model." The proposed structure was created according to the needs of the various groups taking part in the project. The modeling of the structure was carried out through a graphical modeling software where we adapted our concept according to the international standard specification for CubeSats. The parameters verified were weight, dimensions and materials, amongst others. Throughout the development, several prototypes were built in order to verify the technical feasibility of the proposal, enabling improvements to be incorporated in the structure. Comparisons of design and payload volume between the model and the current model were held. From this study it becomes clear that it is an interesting model and very competitive in the conceptual aspect, but for the reliability of that there is the need for further studies such as vibration, thermal and efforts.
Tipo SecundárioPRE CI
AreaETES
Última Atualização dos Metadados2018:06.04.02.40.35 sid.inpe.br/mtc-m21b/2013/09.26.14.25.20 administrator {D 2016}
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Espelhourlib.net/www/2011/03.29.20.55
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Tipo do ConteudoExternal Contribution
Estágio do Documentonot transferred
Permissão de Leituraallow from all
Conteúdo da Pasta sourcenão têm arquivos
Conteúdo da Pasta agreement
agreement.html 03/03/2016 09:26 1.0 KiB 
Histórico2016-03-03 12:26:21 :: simone -> administrator ::
2018-06-04 02:40:35 :: administrator -> simone :: 2016
Campos Vaziosaccessionnumber archivingpolicy archivist booktitle callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor format isbn issn keywords label language lineage mark nextedition nexthigherunit notes numberoffiles numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress resumeid rightsholder secondarydate secondarymark serieseditor session shorttitle size sponsor subject targetfile tertiarymark tertiarytype type url versiontype volume
Data de Acesso19 out. 2020
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Tipo da ReferênciaConference Proceedings
Identificador8JMKD3MGP3W34P/3L9KQ92
Repositóriosid.inpe.br/mtc-m21b/2016/03.03.12.09
Metadadossid.inpe.br/mtc-m21b/2016/03.03.12.09.47
Sitemtc-m21b.sid.inpe.br
Chave SecundáriaINPE--PRE/
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Chave de CitaçãoMathiasMatoFincMane:2016:MiPlAn
Autor1 Mathias, Marcio
2 Matos, Gabriel Vilella
3 Finco, Saulo
4 Manea, Silvio
Grupo1
2
3
4 SGP-ETE-INPE-MCTI-GOV-BR
Afiliação1
2
3
4 Instituto Nacional de Pesquisas Espaciais (INPE)
Endereço de e-Mail do Autor1
2
3
4 silvio.manea@inpe.br
TítuloMicrostrip planar antenna for cubesats
Nome do EventoLatin American IAA CubeSat Workshop, 2
Ano2016
Data28 Feb. - 02 Mar.
Localização do EventoFlorianópolis, SC
ResumoThis proposed solution intended to be a low cost radio transmitter system for sending the collected data CubeSat missions. A compact rectangular patch antenna was chosen to provide a low profile, lightweight and robust design, without requiring any moving parts after the satellite deployment in the space. Because its directional characteristics, the expected antenna gain is about 9,0 dBi.
Idiomaen
Tipo SecundárioPRE CI
AreaETES
Última Atualização dos Metadados2018:06.04.02.40.35 sid.inpe.br/mtc-m21b/2013/09.26.14.25.20 administrator {D 2016}
Estágio do Documentoconcluido
Espelhourlib.net/www/2011/03.29.20.55
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Grupo de Usuáriossimone
Grupo de Leitoresadministrator
simone
Visibilidadeshown
Transferível1
Acervo Hospedeirosid.inpe.br/mtc-m21b/2013/09.26.14.25.20
Tipo do ConteudoExternal Contribution
Estágio do Documentonot transferred
Permissão de Leituraallow from all
Conteúdo da Pasta sourcenão têm arquivos
Conteúdo da Pasta agreement
agreement.html 03/03/2016 09:09 1.0 KiB 
Histórico2016-03-03 12:09:47 :: simone -> administrator ::
2018-06-04 02:40:35 :: administrator -> simone :: 2016
Campos Vaziosaccessionnumber archivingpolicy archivist booktitle callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor format isbn issn keywords label lineage mark nextedition nexthigherunit notes numberoffiles numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress resumeid rightsholder secondarydate secondarymark serieseditor session shorttitle size sponsor subject targetfile tertiarymark tertiarytype type url versiontype volume
Data de Acesso19 out. 2020
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Tipo da ReferênciaConference Proceedings
Identificador8JMKD3MGP3W/3LSD8UE
Repositóriosid.inpe.br/plutao/2016/06.14.13.50
Metadadossid.inpe.br/plutao/2016/06.14.13.50.52
Siteplutao.sid.inpe.br
Rótulolattes: 3678026099849524 7 PetitoViCoSaOrFiMa:2016:ElPoSy
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Chave de CitaçãoPetitoViCoSaOrFiMa:2016:ElPoSy
Autor1 Petito, Otávio Moreira
2 Viana Junior, Arnaldo Alves
3 Cordeiro, Demay
4 Santos, Alessandro de Oliveira
5 Orcajo, Tiago Augusto
6 Finco, Saulo
7 Manea, Silvio
Grupo1
2
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7 SGP-ETE-INPE-MCTI-GOV-BR
Afiliação1
2
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7 Instituto Nacional de Pesquisas Espaciais (INPE)
Endereço de e-Mail do Autor1
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7 silvio.manea@inpe.br
TítuloElectrical Power System (EPS)
Nome do EventoIi Iaa Latin American Cubesat Workshop
Ano2016
Título do LivroProceedings
Data2016
Editora (Publisher)IAA-BR-09-06
Localização do EventoFlorianópolis
ResumoThis article discusses the development of a power system, capable of supplying the entire energy demand of the attitude control subsystem, communication, data processing and payload of the CubeSat, Escola de Engenharia Mau´as project. The power system developed is responsible for generating, distribution and control of the entire energy flow of the CubeSat Mau´a. The energy generated by high efficiency aerospace photocells, endowed with the triple junction technology is stored in Ion-Lithium batteries. The distribution of energy is made by three levels of stabilized voltages and regulated in 3.3V, 5V, 12V and there is a unregulated level supplied directly from the battery. In case of failure, a set of redundant power supplies are able to take any of the regulated voltages levels. All control of the power system is performed by a microcontroller, which collects and analyzes data, such as temperature, voltage and current to determine whether the system power will come from major sources or from redundant ones. Through a CAN network, the microcontroller transmits telemetry information to a Data Processing Unit (DPU), which takes more complex decisions involving all the CubeSat subsystems.
Idiomapt
Tipo SecundárioPRE CI
Tipo TerciárioArtigo
FormatoDVD
AreaETES
Última Atualização dos Metadados2018:06.04.23.26.08 dpi.inpe.br/plutao@80/2008/08.19.15.01 administrator {D 2016}
Estágio do Documentoconcluido
Espelhourlib.net/www/2011/03.29.20.55
e-Mail (login)simone
Grupo de Usuárioslattes
Grupo de Leitoresadministrator
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Acervo Hospedeirodpi.inpe.br/plutao@80/2008/08.19.15.01
Tipo do ConteudoExternal Contribution
Estágio do Documentonot transferred
Permissão de Leituraallow from all
Conteúdo da Pasta sourcenão têm arquivos
Conteúdo da Pasta agreementnão têm arquivos
Histórico2016-06-14 13:50:52 :: lattes -> administrator ::
2016-06-15 17:18:05 :: administrator -> simone :: 2016
2016-06-15 17:21:39 :: simone -> administrator :: 2016
2018-06-04 23:26:08 :: administrator -> simone :: 2016
Campos Vaziosaccessionnumber archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor isbn issn keywords lineage mark nextedition nexthigherunit notes numberoffiles numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisheraddress resumeid rightsholder secondarydate secondarykey secondarymark serieseditor session shorttitle size sponsor subject targetfile tertiarymark type url versiontype volume
Data de Acesso19 out. 2020
atualizar 
similares 
Tipo da ReferênciaConference Proceedings
Identificador8JMKD3MGP3W34P/3N35FBP
Repositóriosid.inpe.br/mtc-m21b/2016/12.20.11.41
Metadadossid.inpe.br/mtc-m21b/2016/12.20.11.41.02
Sitemtc-m21b.sid.inpe.br
Chave SecundáriaINPE--PRE/
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Chave de CitaçãoSouzaAlve:2016:AeInAp
Autor1 Souza, João Paulo Estevam de
2 Alves, João Murta
Grupo1 SGP-ETE-INPE-MCTI-GOV-BR
Afiliação1 Instituto Nacional de Pesquisas Espaciais (INPE)
Endereço de e-Mail do Autor1 joao.souza@inpe.br
TítuloLean-integrated management system for sustainability improvement: aerospace industry application
Nome do EventoAerospace Technology Congress
Ano2016
Data11-12 Oct.
Localização do EventoSolna, Stockholm
ResumoThis work addresses the challenges that aerospace organizations faces in incorporating sustainability into their business strategy and operations. In response to such demand, the Integrated Management System (Quality, Environment, Social Responsibility, and Occupational Health and Safety) integrated with Lean Manufacturing presents itself as a competitive response for aerospace organizations to thrive in the industry under the principles of sustainable development. The investigation of the current models used by organizations reveals the use of Integrated Management Systems and Lean Manufacturing in a non integrated and often conflicting form. The objective of this work is to propose a model for the improvement of the corporate sustainability based on the integration of the Integrated Management System (Quality, Environment, Occupational Health and Safety, and Social Responsibility) and Lean Manufacturing System. The proposed model was applied in an organization of the aerospace industry and the implementation of the proposed model has the potential to improve the organization sustainability performance, with a faster and more flexible production, reducing inventory and quality problems, environmental, social responsibility and occupational safety and health problems, in order to make the company more competitive.
Idiomaen
Tipo SecundárioPRE CI
AreaETES
Tamanho16 KiB
Número de Arquivos1
Arquivo AlvoFT2016_Joao_Souza.pdf
Última Atualização2017:01.02.17.40.55 sid.inpe.br/mtc-m21b/2013/09.26.14.25.20 administrator
Última Atualização dos Metadados2018:06.04.02.41.41 sid.inpe.br/mtc-m21b/2013/09.26.14.25.20 administrator {D 2016}
Estágio do Documentoconcluido
É a matriz ou uma cópia?é a matriz
Espelhourlib.net/www/2011/03.29.20.55
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Grupo de Usuáriosself-uploading-INPE-MCTI-GOV-BR
simone
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Acervo Hospedeirosid.inpe.br/mtc-m21b/2013/09.26.14.25.20
Tipo do ConteudoExternal Contribution
Estágio do Documentonot transferred
Tipo de Versãofinaldraft
Permissão de Leituraallow from all
Conteúdo da Pasta sourcenão têm arquivos
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agreement.html 20/12/2016 09:41 1.0 KiB 
Histórico2016-12-20 11:41:20 :: simone -> administrator :: 2016
2018-06-04 02:41:41 :: administrator -> simone :: 2016
Campos Vaziosaccessionnumber archivingpolicy archivist booktitle callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor format isbn issn keywords label lineage mark nextedition nexthigherunit notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress resumeid rightsholder secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url volume
Data de Acesso19 out. 2020
atualizar 
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