端硝基烯烃含能单体结构与性能的仿真分析OA
Simulation analysis on the structure and performance of terminal nitroalkene energetic monomers
针对硝基烯烃含能单体结构与性能关系不明的难题,通过向端硝基烯烃骨架中引入不同含能基团,设计了 15种端硝基烯烃类含能化合物,开展了端硝基烯烃类含能化合物结构与性能仿真研究.分子结构分析表明,分子整体构型受分子间堆积效应与空间位阻共同影响.前线轨道能计算表明含有醚键的H的能隙值最大,分子稳定性最高.引入吸电子基团(—NO2、—ONO2、—N3、—NF2)提高了衍生物的生成热,除化合物C和H外,其余化合物的密度与爆轰性能均明显提升.其中,化合物B和F的爆速(D)和爆压(p)均高于黑索金(RDX)(B:D=9.02 km/s,p=35.02 GPa;F:D=9.78 km/s,p=42.87 GPa;RDX:D=8.76 km/s,p=34.57 GPa),同时表现出良好的稳定性(特性落高h50>38 cm),有望成为有前景的高能钝感硝基类含能黏合剂单体候选者.
To address the challenge of the unclear relationship between the structure and properties of nitroalkene energetic monomers,fifteen terminal nitroalkene high-energy compounds were designed by introducing various energetic functional groups into the terminal nitroalkene skeleton.The structural and performance simulation of terminal nitroalkene energetic compounds was conducted.The analysis of molecular structures indicates that the overall molecular configuration is determined by the synergistic effects of intermolecular packing and steric hindrance.Frontier orbital energy calculations reveal that H containing an ether bond exhibits the largest energy gap,resulting in the highest molecular stability.The introduction of electron-withdrawing groups(—NO2,—ONO2,—N3,—NF2)enhances the HOFs of the derivatives.Additionally,except for compounds C and H,the density and detonation performance of the other compounds improve evidently.Notably,compounds B and F exhibit detonation velocities(D)and pressures(p)exceeding those of RDX(B:D=9.02 km/s,p=35.02 GPa;F:D=9.78 km/s,p=42.87 GPa;RDX:D=8.76 km/s,p=34.57 GPa),along with good stability(specific drop height h50 exceeding 38 cm).These findings suggest that B and F are promising candidates for high-energy,low-sensitivity energetic materials.
段秉蕙;刘宁;窦金康;莫洪昌;谭博军
西安近代化学研究所,陕西西安 710065西安近代化学研究所,陕西西安 710065西安近代化学研究所,陕西西安 710065西安近代化学研究所,陕西西安 710065西安近代化学研究所,陕西西安 710065
航空航天
固体推进剂端硝基烯烃密度泛函能量特性安全性能
solid propellantsterminal nitroalkenedensity functionalenergy characteristicssafety performance
《火箭推进》 2026 (3)
134-146,13
国家自然科学基金(22405207)
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