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首页> 外文期刊>Propellants, Explosives, Pyrotechnics >Radiative Ignition of Fine-Ammonium Perchlorate Composite Propellants
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Radiative Ignition of Fine-Ammonium Perchlorate Composite Propellants

机译:细高氯酸铵复合推进剂的辐射点火

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摘要

Radiative ignition of quasi-homogeneous mixtures of ammonium perchlorate (AP) and hydroxyterminated polybutadiene (HTPB) binder has been investigated experimentally.Solid propellants consisting of fine AP (2 mu m) and HTPB binder (approx 76/24% by mass) were ignited by CO_2 laser radiation.The lower boundary of a goo-go ignition map (minimum ignition time vs.heat flux) was obtained.Opacity was varied by adding carbon black up to 1% by mass.Ignition times ranged from 0.78 s to 0.076 s for incident fluxes ranging from 60 W/cm~2 to 400 W/cm~2.It was found that AP and HTPB are sufficiently strongly
机译:实验研究了高氯酸铵(AP)和羟基封端的聚丁二烯(HTPB)粘合剂的准均质混合物的放射点火,点燃了由细AP(2μm)和HTPB粘合剂(质量约占76/24%)组成的固体推进剂通过CO_2激光辐射,获得了通过/不通过点火图的下边界(最小点火时间与热通量的关系)。通过添加质量百分比为1%的炭黑来改变不透明性。点火时间为0.78 s 60 W / cm〜2至400 W / cm〜2的入射通量为0.076 s,发现AP和HTPB足够强

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