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Effects of orbital ellipticity on collisional disruptions of rubble-pile asteroids

机译:轨道椭圆度对碎石堆小行星碰撞破坏的影响

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摘要

The behavior of debris ejected from asteroids after collisional disruptions has significant implications for asteroid evolution. Analytical approximations of the elliptic restricted three-body system show that the behavior of ejecta varies significantly with the orbital eccentricity and true anomaly of an asteroid. To study these orbital perturbative effects on collision outcomes, we conduct a series of low-speed collision simulations using a combination of an N-body gravity algorithm and the soft-sphere discrete element method. The asteroid is modeled as a gravitational aggregate, which is one of the plausible structures for asteroids whose sizes are larger than several hundreds of meters. To reduce the effect of complicating factors raised by the mutual interaction between post-collision fragments on the outcomes, a low-resolution model and a set of frictionless material parameters are used in the first step of exploration. The results indicate that orbital perturbations on ejecta arising from the eccentricity and true anomaly of the target asteroid at the time of impact cause larger mass loss and lower the catastrophic disruption threshold (the specific energy required to disperse half the total system mass) in collision events. The "universal law" of catastrophic disruption derived by Stewart and Leinhardt (Astrophys. J. Lett. 691:L133-L137, 2009) can be applied to describe the collision outcomes of asteroids on elliptical heliocentric orbits. Through analyses of ejecta velocity distributions, we develop a semi-analytic description of escape speed from the asteroid's surface in an elliptic restricted three-body system and show that resulting perturbations have long-term orbital effects on ejecta and can also have an indirect influence on the velocity field of post-fragments through interparticle collisions. Further exploration with a high-resolution model shows that the long-term perturbative effects systematically increase mass loss, regardless of the target's material parameters and internal configuration, while indirect effect on mass loss is much more complicated and is enhanced when a coarse material or high-porosity model is used.
机译:碰撞破坏后从小行星弹出的碎片行为对小行星的演变具有重要意义。椭圆受限三体系统的解析近似结果表明,射弹的行为随小行星的轨道偏心率和真实异常而显着变化。为了研究这些轨道扰动对碰撞结果的影响,我们结合N体重力算法和软球离散元方法进行了一系列低速碰撞模拟。小行星被建模为重力聚集体,这是大小大于几百米的小行星的合理结构之一。为了减少因碰撞后碎片之间的相互作用而引起的复杂因素对结果的影响,在勘探的第一步中使用了低分辨率模型和一组无摩擦材料参数。结果表明,撞击时目标小行星的偏心距和真实异常引起的射流轨道扰动会导致更大的质量损失,并降低碰撞事件中的灾难性破坏阈值(分散整个系统质量一半所需的比能) 。由Stewart和Leinhardt得出的灾难性破坏的“普遍定律”(Astrophys。J. Lett。691:L133-L137,2009)可用于描述小行星在椭圆日心轨道上的碰撞结果。通过对射流速度分布的分析,我们对椭圆形受限三体系统中小行星表面的逃逸速度进行了半解析描述,并表明所产生的扰动对射流具有长期的轨道影响,并且也可能对射流产生间接影响粒子间碰撞后碎片的速度场。对高分辨率模型的进一步研究表明,不管目标的材料参数和内部配置如何,长期的扰动效应都会系统地增加质量损失,而对质量损失的间接影响则要复杂得多,当材料较粗或高-孔隙率模型。

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