• Title/Summary/Keyword: 수산기말단 폴리에테르

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Slow Cook-Off Test and Evaluation for HTPE Insensitive Propellants (HTPE 둔감추진제 완속가열 시험평가)

  • Yoo, Ji-Chang;Lee, Do-Hyung;Kim, Chang-Kee;Jung, Jung-Young;Kim, Jun-Hyung;Seo, Tae-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.05a
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    • pp.155-158
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    • 2009
  • This study was investigated to know the thermal decomposition and measure the reaction time and temperature by EIDS cook-off test for the propellant ingredients and 2 kinds of HTPE propellants. The thermal analysis of the propellant ingredients used in this study showed that the thermal stability of these materials decreases in the following order : AP > HTPE > AN > BuNENA. In addition, propellant HTPE 002 containing AN showed that an endothermic process at around $125^{\circ}C$ corresponding to the solid`solid phase change($II{\rightarrow}I$) of AN was followed by the exothermic process due to decomposition of BuNENA/AN until $200^{\circ}C$. HTPE 001 and HTPE 001 reacted at around $250^{\circ}C$ and $152^{\circ}C$ each other, and the temperature of them sharply increased at $115^{\circ}C$ from EIDS slow cook-off tests.

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Slow Cook-Off Test and Evaluation for HTPE Insensitive Propellants (HTPE 둔감추진제 완속가열 시험평가)

  • Yoo, Ji-Chang;Kim, Chang-Kee;Kim, Jun-Hyung;Lee, Do-Hyung;Min, Byung-Sun
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.6
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    • pp.31-37
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    • 2010
  • This study was carried out to investigate the thermal decomposition and execute EIDS slow cook-off test for the propellant ingredients and 2 kinds of HTPE propellants. The thermal analysis of the propellant ingredients used in this study showed that the thermal stability of these materials decreases in the following order : AP > HTPE > AN > BuNENA. In addition, propellant HTPE 002 containing AN showed that an endothermic process at around $125^{\circ}C$ corresponding to the solid phase change(II$\rightarrow$I) of AN was followed by the exothermic process of BuNENA/AN mixture up to $200^{\circ}C$. In EIDS slow cook-off tests, HTPE 001 and HTPE 002 reacted at around $250^{\circ}C$ and $152^{\circ}C$ respectively, and both of them showed sudden temperature increase curves at $115^{\circ}C$. The critical temperatures, $T_c$, of thermal explosion for the propellants HTPE 001 and HTPE 002, were obtained from both the non-isothermal curves at various heating rates and Semenov's thermal explosion theory. Kissinger's method that was used to calculate $T_c$ was also employed to obtain the activation energies for thermal decompositions.