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Prediction of Erosive Wear by Exhaust-Blown Lunar Dust through Experimentally-Validated Computational Modeling

机译:通过实验验证的计算模型预测吹月尘产生的侵蚀磨损

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NASA's Apollo 12 mission provided evidence that lunar dust, accelerated by the exhaust plumes of landing spacecraft, is capable of causing erosive wear damage to nearby lunar structures. During Apollo 12, the Surveyor III lunar probe was "sandblasted" by lunar dust particles advected by the exhaust plume of the Lunar Lander. The low gravitational field of the Moon and the negligible atmospheric drag mean that such lunar dust is able to travel unimpeded for long distances. As a result, lunar structures located far from the spacecraft's landing site are susceptible to such erosive wear damage. In particular, optical instruments, such as lenses and mirrors, and thermal devices, such as radiators, can be severely affected by such particle impingement. Though the particles may not remove much material, their impacts change the object's surface characteristics which, in previous works, the authors have proven can lead to significant changes in reflectance and transmittance. The experimental investigations the authors have done on this subject in previous works with the JSC-1AF lunar dust simulant has been used to validate the computational model in the current work. The model uses the discrete element method (DEM) and computational fluid dynamics (CFD) to predict the motion and impingement of the lunar dust particles. In this study, lunar dust erosive wear of steel, aluminum and acrylic surfaces, and the effect of 30° and 90° impact angles were simulated. A Hertzian contact formulation was used to predict the indentation of the particles into the surface. It was found that the modeling approach is very well-suited to quantitatively predict the erosive wear on the materials simulated. The results from the model agreed with the experiments in the volume of material removed. Also, the shape of the particle impact region matched very well to the experiments. Such physics-based, quantitative modeling approaches for this phenomenon are important as they can help to indentify methods and materials which may be used to mitigate the effects of lunar dust erosive wear. Modeling can also be helpful for obtaining information about low-gravity, thermally-extreme environments which may be challenging to access experimentally. The Moon will see an unprecedented number of lunar landings in the next few years. The exhaust-blown dust by these spacecraft may be become a significant factor affecting the ability for these missions to succeed.
机译:美国宇航局的阿波罗12号飞行任务提供了证据,证明着陆飞船的尾气加速了月尘,能够对附近的月球结构造成腐蚀磨损。在阿波罗12号期间,Surveyor III月球探测器被月球着陆器的尾气流平移的月球尘埃粒子“喷砂”。月球的低引力场和可忽略的大气阻力意味着这种月尘能够无阻碍地长距离传播。结果,远离航天器着陆点的月球结构容易受到这种侵蚀性磨损的损害。尤其是,光学仪器,例如透镜和镜子,以及热装置,例如散热器,可能会受到这种粒子撞击的严重影响。尽管这些颗粒可能不会去除很多物质,但它们的影响会改变物体的表面特性,在以前的工作中,作者证明了这种现象会导致反射率和透射率发生重大变化。作者在先前的工作中就该主题进行了实验研究,其中JSC-1AF月尘模拟物已用于验证当前工作中的计算模型。该模型使用离散元素方法(DEM)和计算流体动力学(CFD)来预测月球尘埃粒子的运动和撞击。在这项研究中,模拟了钢,铝和丙烯酸表面的月尘侵蚀,以及30°和90°冲击角的影响。赫兹接触配方用于预测颗粒进入表面的压痕。结果发现,建模方法非常适合于定量预测模拟材料的侵蚀磨损。该模型的结果与实验的材料去除量相符。而且,粒子撞击区域的形状与实验非常吻合。这种针对这种现象的基于物理的定量建模方法非常重要,因为它们可以帮助确定可用于减轻月尘侵蚀侵蚀的方法和材料。建模还有助于获取有关低重力,热极端环境的信息,这可能很难通过实验获得。在接下来的几年中,月球将出现前所未有的登月次数。这些航天器排出的吹尘可能成为影响这些任务成功的重要因素。

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