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Experimental determination of blast wave pressure loading, thermal radiation protection, and electrical transmission loss for parabolic antenna models in simulated nuclear blast environments.

机译:在抛物面天线模型的模拟核爆炸环境中,对爆炸波压力载荷,热辐射防护和电传输损耗进行实验确定。

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A twelve inch diameter parabolic antenna model instrumented with eleven differential pressure sensors was tested at the Ballistics Research Laboratory of the United States Army Aberdeen Proving Ground, Maryland. Transient pressure loading was determined for 37 different antenna model angular positions with respect to the direction of the blast wave at a peak overpressure of 3.0 pounds per square inch; limited data at 4.5 and 6.0 pounds per square inch were also investigated. The first millisecond of shock wave interaction with the antenna model features the most prominent fully reversed triangular pressure pulse. A blast function, F, was developed that accurately approximates the transient behavior of the blast wave resultant force and moment loading on the antenna model. The resultant blast force on the antenna model is minimized when the axis of the paraboloid of the model is rotated 82 degrees with respect to the direction of the blast wave.; Four different thermal protective coatings were tested at the Ballistics Research Laboratory to evaluate the effects of coating color and thickness. A rating system was developed that evaluates the coatings with respect to thermal performance, coating thickness, material cost, durability, weatherability, maintainability, application cost, color selection and the ability to successfully withstand more than one thermal exposure. The white fluoroelastomer coatings, Caapcoat 1 and Caapcoat 2, achieved the highest overall rating; followed by the ablative char former, Ocean 477; colored versions of Caapcoat 2; and the ceramic tile, Cerez.; Transmission loss measurements were completed on eight different quartz-polyimide antenna models coated with Caapcoat and Ocean 477 thermal protective coatings to measure the changes in transmission loss characteristics. Swept frequency measurements were completed at three different angles of incidence before and after thermal testing across the Super High Frequency, SHF, portion of the electromagnetic frequency spectrum (7.0-8.5 {dollar}times{dollar} 10{dollar}sp9{dollar} cycles per second). The white fluoroelastomer coatings exhibited a two way transmission loss change of approximately 0.20 dB. The ablative char forming coatings exhibited a two way transmission loss of approximately 6.70 dB. Transmission loss measurements were also completed for different types of ablative char formation on Ocean 477 and for an uncoated antenna model.
机译:在马里兰州美国阿伯丁试验场的弹道研究实验室测试了装有11个差压传感器的直径为12英寸的抛物线天线模型。确定了相对于爆炸波方向的37个不同天线模型角位置的瞬态压力负载,峰值过压为3.0磅/平方英寸;还研究了每平方英寸4.5和6.0磅的有限数据。冲击波与天线模型相互作用的第一毫秒具有最突出的完全反转的三角压力脉冲。开发了爆炸函数F,它可以精确地近似爆炸波合力的瞬态行为和天线模型上的力矩载荷。当模型抛物面的轴线相对于爆炸波方向旋转82度时,天线模型上产生的爆炸力最小。在弹道研究实验室测试了四种不同的热防护涂层,以评估涂层颜色和厚度的影响。开发了一种评估系统,可评估涂层的热性能,涂层厚度,材料成本,耐用性,耐候性,可维护性,应用成本,颜色选择以及成功承受多种热暴露的能力。白色含氟弹性体涂料Caapcoat 1和Caapcoat 2达到了最高的总体评级。其次是烧蚀的成炭剂,海洋477; Caapcoat 2的彩色版本;还有瓷砖Cerez。在涂覆有Caapcoat和Ocean 477热保护涂层的八种不同石英-聚酰亚胺天线模型上完成了传输损耗的测量,以测量传输损耗特性的变化。在超高频SHF电磁频谱的一部分(7.0-8.5 {dolal} times {dollar} 10 {dollar} sp9 {dollar}个周期)进行热测试之前和之后,以三个不同的入射角完成了扫频测量每秒)。白色含氟弹性体涂层的双向传输损耗变化约为0.20 dB。烧蚀成炭涂层表现出大约6.70 dB的双向传输损耗。还针对Ocean 477上不同类型的烧蚀性炭和未镀膜天线模型完成了传输损耗测量。

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