Thermal degradation of a composite solid propellant examined by DSC kinetic study

Journal of Thermal Analysis and Calorimetry

Volumn 75, Issue 2, 2004, Pages 551-557

  Rocco, J A F F ^a   Lima, J E S ^a   Frutuoso, A G ^a   Iha, K ^a   Ionashiro, M ^b   Matos, J R ^c   Suarez Iha M E V ^c  

^a INSTITUTO TECNOLÓGICO DE AERONÁUTICA   (Brazil)

^b SÃO PAULO STATE UNIVERSITY UNESP   (Brazil)

^c UNIVERSITY OF SÃO PAULO   (Brazil)

Author keywords

AP HTPB; Differential scanning calorimetry; Kinetic parameters; Ozawa method

Indexed keywords

ACTIVATION ENERGY; COMPOSITE MATERIALS; COMPUTER AIDED SOFTWARE ENGINEERING; COMPUTER SIMULATION; DIFFERENTIAL SCANNING CALORIMETRY; HEATING; NITROGEN; POLYBUTADIENES; PYROLYSIS; REACTION KINETICS; SOLID PROPELLANTS;

ARRHENIUS PARAMETERS; COMPOSITE SOLID PROPELLANT; EXOTHERMIC REACTION KINETICS; KINETIC SHIMADZU SOFTWARE; KISSINGER METHOD; OZAWA METHOD;

AMMONIUM COMPOUNDS;

EID: 1442314805     PISSN: 13886150     EISSN: None     Source Type: Journal    
DOI: 10.1023/B:JTAN.0000027145.14854.f0     Document Type: Article

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