Static Firing Tests of Solid Propellant Rocket Motors: Uncertainty Levels of Thrust Measurements

Detalhes bibliográficos
Autor(a) principal: Fernandes,Fernando Augusto Catalano
Data de Publicação: 2022
Outros Autores: Souto,Carlos d’Andrade, Pirk,Rogério
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Journal of Aerospace Technology and Management (Online)
Texto Completo: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462022000100316
Resumo: ABSTRACT Static firing tests of solid propelled rocket motors (SRMs) are important tests in aerospace industry during the development of new motors as well as to assure the quality of a motor batch. This type of test allows the operator to obtain the measured “thrust versus time of burning” graphic yielded by the motor during burning to verify whether the motor performance matches the project requirements. Laboratory Quality Certificates and good measurement practices make necessary the evaluation of the typical uncertainty of these test results, which demand a wide number of instruments, called measurement chain. This work aims to present the uncertainty levels expressed to the thrust values gathered during a SRM static firing test for two differently configured measurement chains. In order to estimate the uncertainty of a complete measurement chain, the theories of expanded and combined uncertainties are employed. It was possible to verify that in the analyzed case the use of signal amplifiers increased the measurement uncertainty of the chain.
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spelling Static Firing Tests of Solid Propellant Rocket Motors: Uncertainty Levels of Thrust MeasurementsThrust measurementUncertaintySolid rocket motorABSTRACT Static firing tests of solid propelled rocket motors (SRMs) are important tests in aerospace industry during the development of new motors as well as to assure the quality of a motor batch. This type of test allows the operator to obtain the measured “thrust versus time of burning” graphic yielded by the motor during burning to verify whether the motor performance matches the project requirements. Laboratory Quality Certificates and good measurement practices make necessary the evaluation of the typical uncertainty of these test results, which demand a wide number of instruments, called measurement chain. This work aims to present the uncertainty levels expressed to the thrust values gathered during a SRM static firing test for two differently configured measurement chains. In order to estimate the uncertainty of a complete measurement chain, the theories of expanded and combined uncertainties are employed. It was possible to verify that in the analyzed case the use of signal amplifiers increased the measurement uncertainty of the chain.Departamento de Ciência e Tecnologia Aeroespacial2022-01-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462022000100316Journal of Aerospace Technology and Management v.14 2022reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.1590/jatm.v14.1270info:eu-repo/semantics/openAccessFernandes,Fernando Augusto CatalanoSouto,Carlos d’AndradePirk,Rogérioeng2022-09-08T00:00:00Zoai:scielo:S2175-91462022000100316Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2022-09-08T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Static Firing Tests of Solid Propellant Rocket Motors: Uncertainty Levels of Thrust Measurements
title Static Firing Tests of Solid Propellant Rocket Motors: Uncertainty Levels of Thrust Measurements
spellingShingle Static Firing Tests of Solid Propellant Rocket Motors: Uncertainty Levels of Thrust Measurements
Fernandes,Fernando Augusto Catalano
Thrust measurement
Uncertainty
Solid rocket motor
title_short Static Firing Tests of Solid Propellant Rocket Motors: Uncertainty Levels of Thrust Measurements
title_full Static Firing Tests of Solid Propellant Rocket Motors: Uncertainty Levels of Thrust Measurements
title_fullStr Static Firing Tests of Solid Propellant Rocket Motors: Uncertainty Levels of Thrust Measurements
title_full_unstemmed Static Firing Tests of Solid Propellant Rocket Motors: Uncertainty Levels of Thrust Measurements
title_sort Static Firing Tests of Solid Propellant Rocket Motors: Uncertainty Levels of Thrust Measurements
author Fernandes,Fernando Augusto Catalano
author_facet Fernandes,Fernando Augusto Catalano
Souto,Carlos d’Andrade
Pirk,Rogério
author_role author
author2 Souto,Carlos d’Andrade
Pirk,Rogério
author2_role author
author
dc.contributor.author.fl_str_mv Fernandes,Fernando Augusto Catalano
Souto,Carlos d’Andrade
Pirk,Rogério
dc.subject.por.fl_str_mv Thrust measurement
Uncertainty
Solid rocket motor
topic Thrust measurement
Uncertainty
Solid rocket motor
description ABSTRACT Static firing tests of solid propelled rocket motors (SRMs) are important tests in aerospace industry during the development of new motors as well as to assure the quality of a motor batch. This type of test allows the operator to obtain the measured “thrust versus time of burning” graphic yielded by the motor during burning to verify whether the motor performance matches the project requirements. Laboratory Quality Certificates and good measurement practices make necessary the evaluation of the typical uncertainty of these test results, which demand a wide number of instruments, called measurement chain. This work aims to present the uncertainty levels expressed to the thrust values gathered during a SRM static firing test for two differently configured measurement chains. In order to estimate the uncertainty of a complete measurement chain, the theories of expanded and combined uncertainties are employed. It was possible to verify that in the analyzed case the use of signal amplifiers increased the measurement uncertainty of the chain.
publishDate 2022
dc.date.none.fl_str_mv 2022-01-01
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462022000100316
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dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.1590/jatm.v14.1270
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv text/html
dc.publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
dc.source.none.fl_str_mv Journal of Aerospace Technology and Management v.14 2022
reponame:Journal of Aerospace Technology and Management (Online)
instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
instname_str Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron_str DCTA
institution DCTA
reponame_str Journal of Aerospace Technology and Management (Online)
collection Journal of Aerospace Technology and Management (Online)
repository.name.fl_str_mv Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
repository.mail.fl_str_mv ||secretary@jatm.com.br
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