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Thermal Behavior, Non-isothermal Decomposition Reaction Kinetics of Copper(Ⅱ) Salt of 4-Hydroxy-3,5-dinitropyridine and Its Application in Propellant 被引量:2
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作者 CHENPei ZHAOFeng-qi +5 位作者 LUOyang HURong-zu GAOSheng-li ZHENGYu-mei DENGMin-zhi GAOYin 《Chemical Research in Chinese Universities》 SCIE CAS CSCD 2005年第1期100-103,共4页
The thermal behavior and kinetic parameters of the major exothermic decomposition reaction of the title compound in a temperature-programmed mode were studied by means of TG-DTG and DSC. The critical temperature of th... The thermal behavior and kinetic parameters of the major exothermic decomposition reaction of the title compound in a temperature-programmed mode were studied by means of TG-DTG and DSC. The critical temperature of thermal explosion was calculated. The effect of the title compound on the combustion characteristic of composition modifier double base propellant containing RDX was explored with a strand burner. The results show that the kinetic model function in differential forms, the apparent activation energy(E a) and the pre-exponential factor(A) of the major exothermic decomposition reaction are 3(1-α)[-ln(1-α)] 2/3, 190.56 kJ/mol and 10 13.39 s -1, respectively. The critical temperature of thermal explosion of the compound is 353.08 ℃. The kinetic equation of the major exothermic decomposition process of the title compound at 0.1 MPa could be expressed as dα/dT=10 14.65(1-α)[-ln(1-α)] 2/3 e -2.2920×104/T. As an auxiliary catalyzer, the title compound can help the main catalyzer of lead salt of 4-hydroxy-3,5-dinitropyridine to accelerate the burning rate and reduce the pressure exponent of RDX-CMDB propellant. 展开更多
关键词 Thermal behavior Decomposition kinetics Copper(Ⅱ) salt of 4-hydroxy-3 5-dinitropyridine Application PROPELLANT
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2-羟基和4-羟基-3,5-二硝基吡啶铅盐的热行为、分解机理、非等温分解反应动力学及其在推进剂中的应用 被引量:25
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作者 陈沛 赵凤起 +4 位作者 罗阳 胡荣祖 郑玉梅 邓敏智 高茵 《化学学报》 SCIE CAS CSCD 北大核心 2004年第13期1197-1204,J001,共9页
在程序升温条件下 ,用DSC ,TG ,慢速裂解 /傅里叶红外 ,研究了 2 羟基 3 ,5 二硝基吡啶铅盐 ( 2HDNPPb)和 4 羟基 3 ,5 二硝基吡啶铅盐 ( 4HDNPPb)的热行为、机理和动力学参数 ,提出了它们的热分解机理 ,计算了热爆炸临界温度 ,考... 在程序升温条件下 ,用DSC ,TG ,慢速裂解 /傅里叶红外 ,研究了 2 羟基 3 ,5 二硝基吡啶铅盐 ( 2HDNPPb)和 4 羟基 3 ,5 二硝基吡啶铅盐 ( 4HDNPPb)的热行为、机理和动力学参数 ,提出了它们的热分解机理 ,计算了热爆炸临界温度 ,考察了它们对RDX改性双基推进剂的催化效果 .结果表明 :2HDNPPb和 4HDNPPb主放热分解反应的表观活化能和指前因子值分别为 2 5 2 .3 4kJ·mol-1,10 19.3 0 s-1和 187.3 9kJ·mol-1,10 13 .74s-1.由加热速率 β→ 0的DSC曲线的初始温度 (Te)和峰温 (Tp)算得 2HDNPPb和 4HDNPPb的热爆炸临界温度值分别为 3 2 7.64 ,3 3 6.5 7和 3 2 3 .90 ,3 3 3 .96℃ .2HDNPPb的热稳定性优于4HDNPPb .0 .1MPa时 ,它们的放热分解过程动力学方程可表示为 :  对 2HDNPPb  dα/dT =10 2 0 .48( 1-α) [-ln( 1-α) ] 3 /5e-3 .0 3 51× 10 4 /T  对 4HDNPPb  dα/dT =10 15.0 0 ( 1-α) [-ln( 1-α) ] 2 /3 e-2 .2 53 9× 10 4 /T对含RDX改性双基推进剂 ,它们都具有催化燃烧和降低压力指数的作用 .2HDNPPb的催化效果明显优于 4HDNPPb . 展开更多
关键词 2-羟基-3 5-二硝基吡啶铅盐 4-羟基-3 5-二硝基吡啶铅盐 热行为 分解机理 非等温反应动力学 推进剂 含能材料
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2HDNPPb恒容燃烧能的测定及其在RDX-CMDB推进剂中的应用 被引量:6
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作者 赵凤起 高红旭 +3 位作者 罗阳 宋秀铎 郝海霞 李上文 《固体火箭技术》 EI CAS CSCD 北大核心 2005年第4期280-283,共4页
利用精密转动弹热量计测定了2-羟基-3,5-二硝基吡啶铅盐(2HDNPPb)的燃烧能ΔcU,其结果为(-7 265.08±3.97)J/g。据此计算的标准摩尔燃烧焓和标准摩尔生成焓分别为(-4 425.81±2.43)kJ/mol和(-870.47±2.76)kJ/mol。利用均... 利用精密转动弹热量计测定了2-羟基-3,5-二硝基吡啶铅盐(2HDNPPb)的燃烧能ΔcU,其结果为(-7 265.08±3.97)J/g。据此计算的标准摩尔燃烧焓和标准摩尔生成焓分别为(-4 425.81±2.43)kJ/mol和(-870.47±2.76)kJ/mol。利用均匀设计法,研究了2HDNPPb、2-羟基-3,5-二硝基吡啶铜盐(2HDNPCu)和炭黑(CB)在RDX-CMDB推进剂燃烧中的复合催化作用,发现当3种组分的加入量分别为1.0%、0.6%和0.6%时,推进剂在所测压强范围内有最高燃速,并且压强指数较低。 展开更多
关键词 2-羟基-3 5-二硝基吡啶铅盐 含能催化剂 燃烧能 RDX-CMDB推进剂
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Thermal Decomposition Behavior and Non-isothermal Decom-position Reaction of Copper(II) Salt of 4-Hydroxy-3,5-dinitro- pyridine Oxide and Its Application in Solid Rocket Propellant 被引量:2
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作者 陈沛 赵凤起 +5 位作者 罗阳 胡荣祖 高胜利 郑玉梅 邓敏智 高茵 《Chinese Journal of Chemistry》 SCIE CAS CSCD 2004年第9期1056-1063,共8页
The thermal decomposition behavior and kinetic parameters of the exothermic decomposition reactions of the title compound in a temperature-programmed mode have been investigated by means of DSC, TG-DTG and lower rate ... The thermal decomposition behavior and kinetic parameters of the exothermic decomposition reactions of the title compound in a temperature-programmed mode have been investigated by means of DSC, TG-DTG and lower rate thermolysis/FTIR. The possible reaction mechanism was proposed. The critical temperature of thermal explo-sion was calculated. The influence of the title compound on the combustion characteristic of composite modified double base propellant containing RDX has been explored with the strand burner. The results show that the kinetic model function in differential form, apparent activation energy Ea and pre-exponential factor A of the major exo-thermic decomposition reaction are 1-a, 207.98 kJmol-1 and 1015.64 s-1, respectively. The critical temperature of thermal explosion of the compound is 312.87 ℃. The kinetic equation of the major exothermic decomposition process of the title compound at 0.1 MPa could be expressed as: ()416.422.502?d101 edTTaa-10=-. As an auxiliary catalyst, the title compound can help the main catalyst lead salt of 4-hydroxy-3,5-dinitropyridine oxide to en-hance the burning rate and reduce the pressure exponent of RDX-CMDB propellant. 展开更多
关键词 decomposition copper(II) salt of 4-hydroxy-3 5-dinitropyridine oxide kinetics mechanism appli-cation propellant
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