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Experimental Study of Thermal Physical Property of Aged AP/HTPB Composite Base Bleed Propellant
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(1. Nanjing University of Science & Technology,Nanjing 210094, China; 2. 41st Branch of Sixth Research Institute of Aerospace Industry and Technology, Huhehaote 010010, China)

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    Abstract:

    To research the ignition and combustion characteristics of base bleed propellant in the base bleed unit and improve the accuracy of numerical simulation, the specific heat capacity and conductivity coefficient for unaged and naturally aged (stored in a sealed plastic bag under room temperature) AP/HTPB base bleed propellant used in a 155mm base bleed projectile were determined by differential scanning calorimeter (DSC) and conductometer, respectively. Results show that the maximum endothermic peak temperature and the maximum exothermlic peak temperature on DSC curve of the aged base bleed propellant at a heating rate of 20 ℃·min-1 are 253.52 ℃ and 437.54 ℃, respectively. The function of specific heat capacity as temperature with in 40-180 ℃ is obtained based on DSC curves by polynomial fitting method. The average specific heat capacity and conductivity coefficient are 0.9868 kJ·kg-1·℃-1 and 0.2292 W·m-1·K-1 for the aged base bleed propellant and 0.8887 kJ·kg-1·℃-1and 0.4020 W·m-1·K-1 for unaged base bleed propellant, respectively. In comparison with unaged base bleed propellant, the average specific heat capacity of aged base bleed propellant increases about 11%, whereas conductivity coefficient of aged bleed propellant decreases about 43%.

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张领科,赵威,余永刚. AP/HTPB老化复合底排推进剂热物性实验研究[J].含能材料,2014,22(5):669-673.
ZHANG Ling-ke, ZHAP Wei, YU Yong-gang. Experimental Study of Thermal Physical Property of Aged AP/HTPB Composite Base Bleed Propellant[J]. Chinese Journal of Energetic Materials,2014,22(5):669-673.

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History
  • Received:November 27,2013
  • Revised:January 10,2014
  • Adopted:February 24,2014
  • Online: October 29,2014
  • Published: