火炸药学报
火炸藥學報
화작약학보
CHINESE JOURNAL OF EXPLOSIVES & PROPELLANTS
2015年
4期
71-75
,共5页
刘厅%陈昕%胥会祥%韩爱军%叶明泉%杜慧%潘功配
劉廳%陳昕%胥會祥%韓愛軍%葉明泉%杜慧%潘功配
류청%진흔%서회상%한애군%협명천%두혜%반공배
物理化学%硼粉%燃烧性能%富燃料推进剂%镁/聚四氟乙烯%Mg/PTFE
物理化學%硼粉%燃燒性能%富燃料推進劑%鎂/聚四氟乙烯%Mg/PTFE
물이화학%붕분%연소성능%부연료추진제%미/취사불을희%Mg/PTFE
physical chemistry%boron powder%combustion performance%fuel-rich propellant%Mg/PTFE
为研究硼粉含量对镁/聚四氟乙烯(Mg/PTFE)富燃料推进剂性能的影响,采用混合模压成型工艺制备了7种不同硼粉含量的 Mg/PTFE推进剂药柱。用红外测温仪、TG-DTA、量热仪分别测试其燃烧性能、热分解性能和爆热,并测试了其机械感度。结果表明,加入硼粉后,推进剂的燃烧性能明显改善,硼粉质量分数为15%时,线性燃速和质量燃速达到最高;当硼粉质量分数为20%时,燃烧温度达到最高;随着硼粉含量的增加,爆热稍微降低,完全燃烧热随着硼粉含量的增加而增大;当硼粉质量分数为10%时,高温放热峰温度降低128℃,撞击感度和摩擦感度达到最高值。
為研究硼粉含量對鎂/聚四氟乙烯(Mg/PTFE)富燃料推進劑性能的影響,採用混閤模壓成型工藝製備瞭7種不同硼粉含量的 Mg/PTFE推進劑藥柱。用紅外測溫儀、TG-DTA、量熱儀分彆測試其燃燒性能、熱分解性能和爆熱,併測試瞭其機械感度。結果錶明,加入硼粉後,推進劑的燃燒性能明顯改善,硼粉質量分數為15%時,線性燃速和質量燃速達到最高;噹硼粉質量分數為20%時,燃燒溫度達到最高;隨著硼粉含量的增加,爆熱稍微降低,完全燃燒熱隨著硼粉含量的增加而增大;噹硼粉質量分數為10%時,高溫放熱峰溫度降低128℃,撞擊感度和摩抆感度達到最高值。
위연구붕분함량대미/취사불을희(Mg/PTFE)부연료추진제성능적영향,채용혼합모압성형공예제비료7충불동붕분함량적 Mg/PTFE추진제약주。용홍외측온의、TG-DTA、량열의분별측시기연소성능、열분해성능화폭열,병측시료기궤계감도。결과표명,가입붕분후,추진제적연소성능명현개선,붕분질량분수위15%시,선성연속화질량연속체도최고;당붕분질량분수위20%시,연소온도체도최고;수착붕분함량적증가,폭열초미강저,완전연소열수착붕분함량적증가이증대;당붕분질량분수위10%시,고온방열봉온도강저128℃,당격감도화마찰감도체도최고치。
In order to study the effect of content of boron powder on the properties of Mg/PTFE fuel-rich propellant,seven kinds of Mg/PTFE fuel-rich propellants with different contents of boron powder were prepared by mixed proceeding and molding technology.The combustion behaviors,thermal decomposition properties,explosion heat were tested by infrared thermometer,TG-DTA and calorimeter.Their friction and impact sensitivities were also tested.The results show that the combustion behavior of the propellant is significantly improved with the addition of boron.The linear burning rate and mass burning rate reach the maximum when the mass fraction of boron powder is 15%,while the burning temperature reach the maximum when the content of boron powder is 20%.The explosion heat of the propellant decreases with the increase of the boron powder but the whole combustion heat is increased.The impact sensitivity and friction sensitivity of the propellant reach the highest level and the high exothermic temperature peak decreases by 128℃ when the content of boron powder is 10%.