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AP/二茂铁衍生物混合体系的热感度研究 被引量:7

Study on thermal sensitivity of AP and ferrocene derivative mixtures
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摘要 通过局部热感度试验和DSC-TG联用仪,研究了高氯酸铵(AP)和一种二茂铁衍生物(EMT)混合体系的热感度。结果表明,减小AP粒度或增加EMT含量,能缩小AP高低温分解峰之间的差距,提高AP低温分解量,混合物的局部热感度增加。AP存在下,EMT的侧链容易发生断裂,断裂后的二茂铁或二茂铁离子活性体对AP分解起催化作用。此外,EMT不利于AP的质子转移过程,但对HC lO4的分解有较强催化作用。 Thermal sensitivity of AP and ferrocene derivative(EMT) mixtures was studied by partial thermal sensitivity and DSC-TG coupling.The results indicate that reducing AP particle size or increasing the content of EMT can shorten the gap between high-temperature thermal decomposition peak of AP and low-temperature thermal decomposition peak of AP,enhance the low-temperature thermal decomposition amount of AP,and increase partial thermal sensitivity about mixtures of AP and EMT.In the presence of AP,side-chain of EMT is easily ruptured.Residual main skeleton,ferrocene or ferrocene ion,is the real catalyst to thermal decomposition of AP.Furthermore,EMT inhabits proton transfer process of AP,but it is a strong catalysis of EMT to decomposition of HClO4,one of initial decomposition product of AP.
出处 《固体火箭技术》 EI CAS CSCD 北大核心 2011年第2期207-210,共4页 Journal of Solid Rocket Technology
关键词 高氯酸铵 二茂铁衍生物 局部热感度 热分解 AP ferrocene derivative partial thermal sensitivity thermal decomposition
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  • 1刘学,胡期伟.低危险性高燃速推进剂国内外技术发展动态及对未来发展的建议[C]..第二届固体推进剂安全技术研讨会暨固体推进剂生产安全协会第四届代表大会论文集.,2009..
  • 2Strahle W C,Handley J C,Milkie T T.Catalytic effects in the combustion of AP-HTPB sandwiches to 3 200 psia[R].AIAA 72-1120.
  • 3Munson W O,McGee L R,Walker R B.Burning rate modifier effects on a high rate tactical propellant[R].AIAA 77-928.
  • 4Nguyen T T.The effects of ferrocenic and carborane derivative burn rate catalysts in AP composite propellant combustion; mechanism of ferrocene-catalysed combustion[R].DS TO-TR-0121,1995.
  • 5徐浩星,鲁国林,赵秀媛.含燃速催化剂的丁羟推进剂高压燃烧性能研究[J].推进技术,1999,20(3):81-85. 被引量:10
  • 6Pearson G S and Sutton D.Composite solid propellant ignition; ignition of ammonia and other fuels by perchloric acid vapor[J].AIAA,1966,4(5):954-956,also 1967,5(2):344-346,also 1968,7(4):770-771.
  • 7Pittman C U.Location of action of burning-rate catalysts in composite propellant combustion[J].AIAA,1969,7(2); 328-334.
  • 8Hall A R and I 'Anson A C.Experiments with ammonia flames to explore the mode of action of solid composite propellant catalysts[R].AIAA 75-235.
  • 9张炜 朱慧 张仁.AP/HTPB推进剂中过渡金属氧化物催化作用的研究.兵工学报,1990,:23-29.
  • 10Rosser W A,Fishman N and Wise H.Ignition of simulated propellants based on ammonium perchlorate[R].Astia AD 619067.

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