固体火箭技术
固體火箭技術
고체화전기술
JOURNAL OF SOLID ROCKET TECHNOLOGY
2015年
3期
392-395
,共4页
刘亚静%莫洪昌%陈斌%张丽洁%高福磊%姬月萍
劉亞靜%莫洪昌%陳斌%張麗潔%高福磊%姬月萍
류아정%막홍창%진빈%장려길%고복뢰%희월평
有机化学%有机合成%三(叠氮乙酰氧甲基)硝基甲烷%性能
有機化學%有機閤成%三(疊氮乙酰氧甲基)硝基甲烷%性能
유궤화학%유궤합성%삼(첩담을선양갑기)초기갑완%성능
organic chemistry%organic synthesis%TMNTA%property
以三羟甲基硝基甲烷为原料,经酯化、叠氮化两步反应合成出三(叠氮乙酰氧甲基)硝基甲烷,总收率为83.0%。利用红外光谱、核磁共振、元素分析表征了其结构。探讨了叠氮化反应的影响因素,确定其最佳反应条件为:NaN3摩尔加入量为理论值的1.10倍,混合溶剂中水占总体积的10%~25%,反应时间1 h。测试得到TMNTA的密度为1.45 g/cm3,热分解温度为235.7℃,玻璃化转变温度为-26.23℃,撞击感度H50=44.7 cm(落锤2 kg),爆炸概率4%(摆角66°)。
以三羥甲基硝基甲烷為原料,經酯化、疊氮化兩步反應閤成齣三(疊氮乙酰氧甲基)硝基甲烷,總收率為83.0%。利用紅外光譜、覈磁共振、元素分析錶徵瞭其結構。探討瞭疊氮化反應的影響因素,確定其最佳反應條件為:NaN3摩爾加入量為理論值的1.10倍,混閤溶劑中水佔總體積的10%~25%,反應時間1 h。測試得到TMNTA的密度為1.45 g/cm3,熱分解溫度為235.7℃,玻璃化轉變溫度為-26.23℃,撞擊感度H50=44.7 cm(落錘2 kg),爆炸概率4%(襬角66°)。
이삼간갑기초기갑완위원료,경지화、첩담화량보반응합성출삼(첩담을선양갑기)초기갑완,총수솔위83.0%。이용홍외광보、핵자공진、원소분석표정료기결구。탐토료첩담화반응적영향인소,학정기최가반응조건위:NaN3마이가입량위이론치적1.10배,혼합용제중수점총체적적10%~25%,반응시간1 h。측시득도TMNTA적밀도위1.45 g/cm3,열분해온도위235.7℃,파리화전변온도위-26.23℃,당격감도H50=44.7 cm(락추2 kg),폭작개솔4%(파각66°)。
TMNTA was synthesized using tris( hydroxymethyl) nitromethane as raw material,via the two?step reactions of esterif?ication, azidonation with a total yield of 83.0%.Its structures were confirmed by IR,NMR and elemental analysis.The affecting fac?tors of azidonation were studied.The optimum conditions of the reactions were:nexp:ntheory=1.10 for NaN3(molar ratio),10%~25% of the total volume of acetone?H2 O and reaction time 1 h. Some physicochemical properties of TMNTA were obtained by the tests.Results show that the density is 1.45 g/cm3,decomposition temperature is 235.7℃,glass transition temperature is-26.23 ℃, H50=44.7cm(2 kg),friction sensitivity is 4%(66°).