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Experimental study on thermal decomposition kinetics of natural ageing AP/HTPB base bleed composite propellant 被引量:5

Experimental study on thermal decomposition kinetics of natural ageing AP/HTPB base bleed composite propellant
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摘要 The kinetics of the thermal decomposition for a naturally ageing ammonium perchlorate(AP) and hydroxyl-terminated-polybutadiene(HTPB) base bleed composite propellant were investigated using a differential scanning calorimetry(DSC). The naturally ageing AP/HTPB base bleed propellant samples have been stored in a sealed plastic bag at room temperature(5-25 ℃) for more than 20 years. The experimental DSC results were obtained by placing samples(each about 1.5 mg) in a sealed pan under non-isothermal condition under different heating rates, 5.0, 10.0, 15.0, 20.0 and 30.0 ℃·min^(-1). The activation energy and pre-exponential factor were estimated based on the relationship between the exothermic peak temperature and the heating rate by Ozawa and Kissinger methods, respectively. The decomposition kinetic parameters is lower the values under laboratorial aging condition. The kinetics of the thermal decomposition for a naturally ageing ammonium perchlorate(AP) and hydroxyl-terminated-polybutadiene(HTPB) base bleed composite propellant were investigated using a differential scanning calorimetry(DSC). The naturally ageing AP/HTPB base bleed propellant samples have been stored in a sealed plastic bag at room temperature(5-25 ℃) for more than 20 years. The experimental DSC results were obtained by placing samples(each about 1.5 mg) in a sealed pan under non-isothermal condition under different heating rates, 5.0, 10.0, 15.0, 20.0 and 30.0 ℃·min^(-1). The activation energy and pre-exponential factor were estimated based on the relationship between the exothermic peak temperature and the heating rate by Ozawa and Kissinger methods, respectively. The decomposition kinetic parameters is lower the values under laboratorial aging condition.
出处 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2018年第5期422-425,共4页 Defence Technology
关键词 Base bleed technology AP/HTPB composite PROPELLANT NATURAL ageing DECOMPOSITION KINETICS DSC EXPERIMENT Base bleed technology AP/HTPB composite propellant Natural ageing Decomposition kinetics DSC experiment
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  • 1封锋,陈军,郑亚,唐健.高燃速丁羟推进剂燃速可调节性研究[J].弹道学报,2010,22(1):74-78. 被引量:6
  • 2张炎清,赵子华.底部排气弹底排装置点火过程对距离散布的影响[J].弹道学报,1994,6(1):53-56. 被引量:13
  • 3中国人民解放军总装备部.GJB 5413-2005 底部排气弹射表编拟方法[S].北京:中国人民解放军总装备部,2005:27-31.
  • 4Lyle D Kayser, John D Kuzan, David N Vazguez. Flight testing for a 155 mm base burn projectile, AD-A222-562 [ N]. US: DTIC, 1990.
  • 5James E Danberg. Analysis ofthe flight performance of the 155 mm M864 base bsrn projectile, AD-A222-624 [R ]. US: DTIC, 1990.
  • 6吴婉娥,毛根旺,王英红,胡松启.AP含量及粒度级配对含硼富燃推进剂压强指数的影响[J].固体火箭技术,2007,30(4):332-334. 被引量:9
  • 7赵银 田德余 江瑜.AP复合固体推进剂燃烧模型[J].宇航学报,1988,(4):15-22.
  • 8薛毅.最优化原理和方法[M].北京.北京工业大学出版社,2001.269-286.
  • 9GUO K K, SUMMERFIELD M. Fundamentals of solid- propellant combustion [ M ]. Beijing: China Astronautic Publishing House, 1994 .
  • 10贺南昌,王学锋,程根旺.高氯酸铵(AP)粒度对端羟基聚丁二烯(HTPB)推进剂燃烧特性的影响[J].火炸药学报,1984,(6):1-8.

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