固体火箭技术
固體火箭技術
고체화전기술
JOURNAL OF SOLID ROCKET TECHNOLOGY
2009年
5期
539-542,553
,共5页
谢明召%衡淑云%刘子如%王晗%王晓红%赵凤起
謝明召%衡淑雲%劉子如%王晗%王曉紅%趙鳳起
사명소%형숙운%류자여%왕함%왕효홍%조봉기
物理化学%纳米燃速催化剂%热重-差示扫描量热-红外-质谱联用%热分解%RDX-CMDB
物理化學%納米燃速催化劑%熱重-差示掃描量熱-紅外-質譜聯用%熱分解%RDX-CMDB
물이화학%납미연속최화제%열중-차시소묘량열-홍외-질보련용%열분해%RDX-CMDB
physical chemistry%nano burning rate catalyst%TG-DSC-IR-MS%thermal decomposition%RDX-CMDB
采用热重-差示扫描量热-红外-质谱(TG-DSC-IR-MS)联用技术,研究了三元复合燃速催化剂(2,4二羟基苯甲酸铅、对氨基苯甲酸铜和炭黑)对RDX-CMDB推进剂热分解的作用,并比较了纳米和普通催化剂作用效果的差异.结果表明,该复合燃速催化剂使RDX-CMDB推进剂热分解特征量发生明显变化;改变了推进剂中RDX的初期热分解机理,使放热的CN键断裂在与吸热的NNO_2 键断裂的竞争反应中占优;也使双基组分放出有负生成热的CH_2O的相对量增加,分解过程放热量或放热速度提高,促进了燃速的提高.与普通催化剂相比,纳米催化剂作用效果更好.
採用熱重-差示掃描量熱-紅外-質譜(TG-DSC-IR-MS)聯用技術,研究瞭三元複閤燃速催化劑(2,4二羥基苯甲痠鉛、對氨基苯甲痠銅和炭黑)對RDX-CMDB推進劑熱分解的作用,併比較瞭納米和普通催化劑作用效果的差異.結果錶明,該複閤燃速催化劑使RDX-CMDB推進劑熱分解特徵量髮生明顯變化;改變瞭推進劑中RDX的初期熱分解機理,使放熱的CN鍵斷裂在與吸熱的NNO_2 鍵斷裂的競爭反應中佔優;也使雙基組分放齣有負生成熱的CH_2O的相對量增加,分解過程放熱量或放熱速度提高,促進瞭燃速的提高.與普通催化劑相比,納米催化劑作用效果更好.
채용열중-차시소묘량열-홍외-질보(TG-DSC-IR-MS)련용기술,연구료삼원복합연속최화제(2,4이간기분갑산연、대안기분갑산동화탄흑)대RDX-CMDB추진제열분해적작용,병비교료납미화보통최화제작용효과적차이.결과표명,해복합연속최화제사RDX-CMDB추진제열분해특정량발생명현변화;개변료추진제중RDX적초기열분해궤리,사방열적CN건단렬재여흡열적NNO_2 건단렬적경쟁반응중점우;야사쌍기조분방출유부생성열적CH_2O적상대량증가,분해과정방열량혹방열속도제고,촉진료연속적제고.여보통최화제상비,납미최화제작용효과경호.
Thermal decomposition of RDX-CMDB propellants with composite burning rate catalysts (β-Pb、PAC and CB) were investigated by using on-line TG-DSC-IR-MS techniques. On the basis of changes in main gaseous products, the influence of the nano and general catalysts on the characteristic values of thermal decomposition was compared and effect mechanism of catalysts was discussed. It is shown that the addition of composite burning catalysts changes the characteristic values of thermal decomposition obviously and the initial decomposition mechanism of RDX. The C-N bond split as an exothermic process has a predominance over competing branch reaction N-NO_2 bond split as an endothermic process. The relative quantity of CH_2O (with negative forming heat) produced from the decomposition of NC/NG component increases. Because of the decomposition heat or heat release rate increases, the burning rate of propellants increases. The effect of nano catalysts is better than that of general catalysts.