dc.contributorSão José Dos Campos
dc.contributorUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2014-05-27T11:30:31Z
dc.date.available2014-05-27T11:30:31Z
dc.date.created2014-05-27T11:30:31Z
dc.date.issued2013-09-01
dc.identifierJournal of Thermal Analysis and Calorimetry, v. 113, n. 3, p. 1209-1216, 2013.
dc.identifier1388-6150
dc.identifierhttp://hdl.handle.net/11449/76386
dc.identifier10.1007/s10973-013-2968-8
dc.identifierWOS:000323503300027
dc.identifier2-s2.0-84883139641
dc.identifier8498310891810082
dc.identifier7471310113999140
dc.identifier0000-0002-7984-5908
dc.description.abstractThe propulsion of most of the operating satellites comprises monopropellant (hydrazine - N2H4) or bipropellant (monometilydrazine - MMH and nitrogen tetroxide) chemical systems. When some sample of the propellant tested fails, the entire sample lot shall be rejected, and this action has turned into a health problem due to the high toxicity of N2H 4. Thus, it is interesting to know hydrazine thermal behavior in several storage conditions. The kinetic parameters for thermal decomposition of hydrazine in oxygen and nitrogen atmospheres were determined by Capela-Ribeiro nonlinear isoconversional method. From TG data at heating rates of 5, 10, and 20 C min-1, kinetic parameters could be determined in nitrogen (E = 47.3 ± 3.1 kJ mol-1, lnA = 14.2 ± 0.9 and T b = 69 C) and oxygen (E = 64.9 ± 8.6 kJ mol-1, lnA = 20.7 ± 3.1 and T b = 75 C) atmospheres. It was not possible to identify a specific kinetic model for hydrazine thermal decomposition due to high heterogeneity in reaction; however, experimental f(α)g(α) master-plot curves were closed to F 1/3 model. © 2013 Akadémiai Kiadó, Budapest, Hungary.
dc.languageeng
dc.relationJournal of Thermal Analysis and Calorimetry
dc.relation2.209
dc.relation0,587
dc.rightsAcesso aberto
dc.sourceScopus
dc.subjectHydrazine
dc.subjectNon isothermal kinetic
dc.subjectPropellant
dc.subjectThermal decomposition
dc.subjectDecomposition of hydrazine
dc.subjectHigh heterogeneity
dc.subjectIso-conversional method
dc.subjectNitrogen tetroxide
dc.subjectNon-isothermal kinetic
dc.subjectOxygen and nitrogens
dc.subjectStorage condition
dc.subjectThermal behaviors
dc.subjectDecomposition
dc.subjectDigital storage
dc.subjectKinetic parameters
dc.subjectNitrogen
dc.subjectNitrogen oxides
dc.subjectOxygen
dc.subjectPropellants
dc.subjectPyrolysis
dc.titleKinetic parameters for thermal decomposition of hydrazine
dc.typeActas de congresos


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