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EMPIRICAL CO-RELATION BETWEEN BURN RATE AND PRESSURE INDEX OF SPHERICAL GUN PROPELLANT IN CLOSED BOMB

机译:密闭炸弹中球形火药推进剂的燃烧速率与压力指数的经验关系

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In this research paper, empirical relation between burn rate and pressure index of spherical gun propellant was carried out in the closed bomb. This is double base propellant and used in power cartridge to destroy the suspicious unattended objects. The novelty in this research is that, the author proposed a novel empirical relation among force constant, burning rate coefficient, pressure index and peak pressure. Ballistics properties like burning rate of propellant is depend upon on its shape and size (configuration), chemical composition, temperature, loading density and pressure. The major outcome of this research study has direct relevance for the performance prediction of propellant in the form of powder related to dynamic firings. The peak pressure of the propellant is 235.04 MPa, the rise time 1.95 ms, burn rate coefficient 0.073, pressure index 1.29, flame temperature 2680 ~0K and force constant 953.2 J/g were obtained during experiment. The burning rate for the spherical gun propellant is experimentally expressed as r= 0.073 × 235.04~(1.29)
机译:本文研究了密闭炸弹中球形火药的燃烧速率与压力指数之间的经验关系。这是双基推进剂,用于动力装置中,用于摧毁可疑的无人看管的物体。这项研究的新颖之处在于,作者提出了力常数,燃烧速率系数,压力指数和峰值压力之间的新型经验关系。弹药的性质如推进剂的燃烧速率取决于其形状和大小(构型),化学成分,温度,载荷密度和压力。这项研究的主要成果与与动态点火有关的粉末形式的推进剂性能预测直接相关。推进剂的峰值压力为235.04 MPa,上升时间为1.95 ms,燃烧速率系数为0.073,压力指数为1.29,火焰温度为2680〜0K,力常数为953.2 J / g。球形火炮推进剂的燃烧速率实验表示为r = 0.073×235.04〜(1.29)

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