Design of a Mortar-Deployed Video Imager

J. Condon
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Abstract

As part of a US Army Research Laboratory (Aberdeen Proving Ground, MD) project to provide electromechanical packaging support for a developmental gun-hardened, munition-deployed, parachute-deployed video imager, a dynamic FEA structural analysis was performed on the imager’s aluminum housing. This imager can provide real-time, telemetered, digitally-encrypted and encoded video imaging of the battlefield. The housing was designed as a carrier for the power distribution electronics; video encoding electronics; telemetry transmitter and wrap-around antenna; rechargeable NiCad batteries; and CCD camera module, and provided for direct replacement of an existing illumination canister within a modified US Army 120mm mortar system. The imager assembly, once inserted within the mortar body, is first exposed to a launch ‘setback’ acceleration load upon firing and then is exposed to an explosively-generated internal pressure and impact loading upon in-flight fuze initiation, mortar body separation and subsequent imager submunition expulsion. The dynamic analysis entailed verification of the structural integrity and deflections of the imager housing and adjacent impacting steel ‘pusher’ plate under launching, pressure, and impact loadings. A 2-D axi-symmetric, quadrilateral-only, finite element model of the housing and pusher plate was constructed. Contact elements, birth & death displacement constraints and simplified mortar body elements were added to simulate the boundary conditions. Analysis predictions were validated by inspection of the recovered imager hardware following flight testing.
迫击炮部署视频成像仪的设计
作为美国陆军研究实验室(Aberdeen试验场,MD)项目的一部分,为一种正在开发的火炮硬化、弹药部署、降落伞部署的视频成像仪提供机电包装支持,对成像仪的铝外壳进行了动态有限元结构分析。该成像仪可以提供实时、遥测、数字加密和编码的战场视频成像。外壳被设计为配电电子设备的载体;视频编码电子;遥测发射机及环绕式天线;可充电镍镉电池;和CCD相机模块,并提供直接替换现有的照明筒内的改进的美国陆军120毫米迫击炮系统。成像仪组件一旦插入迫击炮体内,在发射时首先暴露于发射“挫折”加速度载荷,然后暴露于爆炸产生的内部压力和飞行引信启动时的冲击载荷,迫击炮体分离和随后的成像仪子母弹排出。动态分析需要验证成像仪外壳和相邻冲击钢板在发射、压力和冲击载荷下的结构完整性和挠度。建立了壳体和推板的二维轴对称四边形有限元模型。通过加入接触单元、生死位移约束和简化砂浆体单元来模拟边界条件。在飞行测试后,通过检查回收的成像仪硬件,验证了分析预测。
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