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Detection of structure in asteroid analogue materials and Titan’s regolith by a landing spacecraft

机译:通过着陆航天器检测小行星类似物材料和土卫六的风化层中的结构

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摘要

We compare measurements made by two impact penetrometers of different sizes and with different tip shapes to further understand penetrometer design for performing pentrometry on an asteroid. To this end we re-visit the interpretation of data from the Huygens' penetrometer, ACC-E, that impacted Titan's surface. In addition we investigate the potential of a spacecraft fitted with a penetrometer to bounce using a test rig, built at The Open University (UK).udAnalysis of ACC-E laboratory data, obtained from impacts into ~4 mm diameter gravel, was found to produce an unusual decrease in resistance with depth (force-depth gradient) which was also seen in the Huygens' ACCE data from Titan and originally interpreted as a wet or moist sand. The downward trend could also be reproduced in a hybrid Discrete Element Model (DEM) if it was assumed that the near surface particles are more readily mobilised than those deeper in the target.udWith regard to penetrometer design penetration resistance was found to be sensitive to the ratio of particle to tip diameter. A clear trend was observed with a conical tip penetrometer, X-PEN, of decreasing force-depth gradients with increasing particle sizes most likely due to a transformation from a bulk displacement of material by the penetrating tip to more local interactions. ACC-E, which has a hemispherical tip, was found to produce a wider range of force-depth gradients than X-PEN, which had a conical tip, possibly due to difficulties dislodging jammed particles. Both penetrometers were able to determine particle diameter and mass after post-processing of the data.udLaboratory simulations of landings with the test rig suggest that a large impact penetrometer under certain circumstances could absorb a significant amount of the elastic energy of the spacecraft possibly aiding landing. Alternatively a small impact penetrometer would allow the spacecraft to bounce freely on the surface to make a measurement at another location.
机译:我们比较了两个不同尺寸和尖端形状的冲击渗透仪的测量结果,以进一步了解渗透仪在小行星上进行渗透测定的设计。为此,我们再次访问了惠更斯(Huygens)透度计ACC-E的数据,该数据影响了泰坦的表面。此外,我们还使用开放大学(UK)建造的试验台,研究了装有渗透计的航天器弹跳的潜力。 ud分析了撞击到直径约4毫米的砾石后获得的ACC-E实验室数据会随深度(力-深度梯度)产生不同寻常的阻力降低,这在泰坦的惠更斯(Huygens)ACCE数据中也可以看到,最初被解释为潮湿或潮湿的沙子。如果假定近表面粒子比目标深层的粒子更容易动员,则在混合离散元素模型(DEM)中也可以再现下降趋势。 ud关于渗透仪的设计,发现穿透阻力对颗粒与尖端直径之比。锥形尖端渗透仪X-PEN观察到明显的趋势,即力深梯度减小,而粒径增大,这很有可能是由于从尖端的材料整体位移到更多局部相互作用的转变。发现具有半球形尖端的ACC-E比具有锥形尖端的X-PEN产生更大的作用力深度梯度范围,这可能是由于难以清除堵塞的颗粒。在对数据进行后处理之后,这两种渗透仪都能够确定粒径和质量。 ud使用试验台对实验室进行着陆模拟表明,在某些情况下,大型冲击渗透仪可以吸收飞船的大量弹性能,这可能有助于降落。替代地,小的冲击渗透仪将允许航天器在表面上自由弹跳以在另一个位置进行测量。

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