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CHARACTERIZATION OF THE M1020 IGNITION CARTRIDGE UNDER SIMULATED MORTAR FIRING CONDITIONS

机译:模拟砂浆烧制条件下M1020点火盒的表征

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The objective of this study was to investigate the combustion processes of a 120-mm mortar propulsion system under realistic firing conditions for advancing model simulation and performance improvements. Two test rigs were designed to characterize the combustion behavior of the M1020 ignition cartridge alone and with additional aligned and unaligned charge increments. In order to deduce the mass and energy fluxes out of the vent holes, monitor flame spreading through the granular propellant bed, and observe the pressure distribution along the tail boom, tests were conducted on 65∞ elevated tail booms and in an instrumented high-pressure mortar chamber simulator. Results showed that heat-transfer and fluid-flow processes from the discharging combustion products were multi-dimensional, resulting in transverse flame spreading through the granular bed. Also, highly non-uniform radial distributions of pressure near the fins were detected when the charge increments were loaded in an aligned direction, resulting in undesirable fin blade damage.
机译:本研究的目的是在逼真的烧制条件下研究120毫米砂浆推进系统的燃烧过程,以推进模型模拟和性能改进。设计了两个试验台,以表征单独的M1020点火盒的燃烧行为,并具有额外的对准和未对准的充电增量。为了使物质和能量通量从通气孔中推断出来,监测通过粒状推进剂床的火焰蔓延,并观察沿尾部臂的压力分布,在65°升高的尾部动臂上进行测试,并在仪表高压下进行测试砂浆室模拟器。结果表明,来自排出燃烧产物的热传递和流体流动过程是多维的,导致横向火焰通过颗粒床扩散。此外,当充电增量以对准方向上装入翅片时,检测到翅片附近的高度不均匀的径向分布,导致不希望的翅片叶片损坏。

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