Authors:
J. Rocco Aeroespacial São José Instituto Tecnológico de Aeronáutica, Centro Técnico dos Campos, S.P. Brasil

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J. Lima Aeroespacial São José Instituto Tecnológico de Aeronáutica, Centro Técnico dos Campos, S.P. Brasil

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A. Frutuoso Aeroespacial São José Instituto Tecnológico de Aeronáutica, Centro Técnico dos Campos, S.P. Brasil

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K. Iha Aeroespacial São José Instituto Tecnológico de Aeronáutica, Centro Técnico dos Campos, S.P. Brasil

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M. Ionashiro Aeroespacial São José Instituto Tecnológico de Aeronáutica, Centro Técnico dos Campos, S.P. Brasil

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J. Matos Aeroespacial São José Instituto Tecnológico de Aeronáutica, Centro Técnico dos Campos, S.P. Brasil

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M. Suárez-Iha Aeroespacial São José Instituto Tecnológico de Aeronáutica, Centro Técnico dos Campos, S.P. Brasil

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Abstract  

Thermal decomposition kinetics of solid rocket propellants based on hydroxyl-terminated polybutadiene-HTPB binder was studied by applying the Arrhenius and Flynn-Wall-Ozawa's methods. The thermal decomposition data of the propellant samples were analyzed by thermogravimetric analysis (TG/DTG) at different heating rates in the temperature range of 300-1200 K. TG curves showed that the thermal degradation occurred in three main stages regardless of the plasticizer (DOA) raw material, the partial HTPB/IPDI binder and the total ammonium perchlorate decompositions. The kinetic parameters Ea (activation energy) and A (pre-exponential factor) and the compensation parameter (Sp) were determined. The apparent activation energies obtained from different methods showed a very good agreement.

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Journal of Thermal Analysis and Calorimetry
Language English
Size A4
Year of
Foundation
1969
Volumes
per Year
1
Issues
per Year
24
Founder Akadémiai Kiadó
Founder's
Address
H-1117 Budapest, Hungary 1516 Budapest, PO Box 245.
Publisher Akadémiai Kiadó
Springer Nature Switzerland AG
Publisher's
Address
H-1117 Budapest, Hungary 1516 Budapest, PO Box 245.
CH-6330 Cham, Switzerland Gewerbestrasse 11.
Responsible
Publisher
Chief Executive Officer, Akadémiai Kiadó
ISSN 1388-6150 (Print)
ISSN 1588-2926 (Online)

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