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作 者:袁志锋[1] 赵凤起[1] 焦建设 张教强[3] 杨立波[1] 郑晓东[1] 张超[1] 谢波[1]
机构地区:[1]西安近代化学研究所燃烧与爆炸技术重点实验室,陕西西安710065 [2]炮兵防空兵装备技术研究所,北京100012 [3]西北工业大学,陕西西安710072
出 处:《火工品》2014年第4期20-23,共4页Initiators & Pyrotechnics
基 金:国家自然科学基金(21173163);燃烧与爆炸技术重点实验室基金(9140C350341006)
摘 要:为了研究2,4-二羟基苯甲酸铅铜盐(Pb/Cu-SDHB)单独或与其它催化剂复合后对含Al粉和黑索今(RDX)改性双基(AI/RDX-CMDB)推进剂燃烧I生能的影响,采用吸收.压延方法制备了推进剂样品,用靶线法测试了推进剂燃速。结果表明:Pb/Cu-sDHB能有效调节推进剂燃烧性能,显著提高了A1/RDX-cMDB推进剂的燃速,并明显降低了压强指数;3.0%Pb/Cu-SDHB与0.65%炭黑复合后使A1RDX-cMDB推进剂在10~15MPa的压强指数降低至.0.1,10MPaT燃速黜0mm/s。In order to investigate the effects of lead/cupric salt of 2,4-dihydroxybenzoate(Pb/Cu-SDHB)itself, or composite with other catalysts on the combustion properties of AI/RDX-CMDB propellant, the propellant samples were prepared through a solventless extrusion technique, as well as the burning rate of propellants were measured by stand burner method .The results showed that Pb/Cu-SDHB could increase the burning rate and reduce the pressure exponent of AI/RDX-CMDB propellant notably. When 3.0% Pb/Cu-SDHB composited with 0.65% carbon, the pressure exponent of AI/RDX-CMDB propellant reduced to -0.1 under 10~15MPa, and the burning rate at 10MPa would exceed 20mm/s.
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