首页> 外文会议>AIAA/ASME/SAE/ASEE joint propulsion conference >Azidonation derivatives of 1,1',4,4'-tetramethyl-2-tetrazene as nitrogen-rich compounds for NTO/MMH replacement - Synthesis, characterization and properties
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Azidonation derivatives of 1,1',4,4'-tetramethyl-2-tetrazene as nitrogen-rich compounds for NTO/MMH replacement - Synthesis, characterization and properties

机译:1,1',4,4'-四甲基-2-四氮烯作为NTO / MMH替代的氮化合物的叠氮化衍生物为合成,表征和性能

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摘要

Direct α-addition of azido groups on methyltetrazene backbones had never been described in the literature. We report herein the one-step α-azidonation of 1,1',4,4'-tetramethyl-2-tetrazene (TMTZ) that leads to 1-azidomethyl-1',4,4'-trimethyl-2-tetrazene (MATMTZ) and 1,4-di(azidomethyl)-1',4'-dimethyl-2-tetrazene (DADMTZ): two nitrogen-rich tetrazene derivatives with promising energetic interest These compounds were synthesized using azidoiodinane reagents such as the iodosylbenzene/trimethylsilyl azide couple or azidobenziodoxolone, while neither coloration reagents nor sodium azide allowed the introduction of azido groups on the α-carbon of tetramethyltetrazene. The a-azidonation reaction of TMTZ was optimized in order to predominantly form either mono- or di-azidomethyltetrazene derivative, which were characterized by ~1H, °C and ~(15)N NMR. Moreover, the theoretical heats of formation of the two azidoderivatives were computed using Density Functional Theory (B3LYF) and composite methods (CBS-QB3). Propulsion performance parameters such as density and specific impulse were calculated using, respectively, Molecular Mechanics (MM) and OPHELIE code, which is a variant of the CEA code of NASA.
机译:在文献中从未描述过甲基四烯骨架上的Azido基团的直接α-加入。我们报告本文一步法的1,1-α-azidonation' ,4,4'-四甲基-2-四氮烯(TMTZ)通向1-叠氮基甲基-1' ,4,4'-三甲基-2-四氮烯( MATMTZ)和1,4-二(叠氮基甲基)-1' ,4'-二甲基-2-四氮烯(DADMTZ):用高能有为兴趣使用azidoiodinane试剂如亚碘酰苯/三甲基甲硅烷合成这些化合物2的富氮四氮烯衍生物叠氮化物偶联或azidobenziodoxolone,而既不着色试剂,也不叠氮化钠允许在tetramethyltetrazene的α碳的引入叠氮基团。 TMTZ的a azidonation反应是为了优化,以主要形成或者单或二azidomethyltetrazene衍生物,将其特征为〜1H,℃,〜(15)N NMR。此外,形成两个azidoderivatives的理论加热使用密度泛函理论(B3LYF)和复合的方法(CBS-QB3)进行了计算。使用,分别计算推进性能参数,例如密度和比冲,分子力学(MM)和OPHELIE代码,这是NASA的CEA代码的变体。

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