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arXiv 2308.02071astro-ph.EPphysics.space-ph
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重新审视缓解潜在危险小行星撞击问题

Mitigating potentially hazardous asteroid impacts revisited

Zs. Regaly, V. Frohlich, P. Berczik

AI总结:

本研究通过高精度N体模拟,发现轨道剪切使碎片云呈三轴椭球状,其取向决定撞击地球的碎片数量,提出在PHA轨道近心点拦截可最小化撞击后果。

摘要:

背景:位于穿越地球轨道上的潜在危险小行星(PHA)对地球生命构成持续威胁。目前已提出多种缓解方法,其中最具可行性的技术似乎是在拦截时通过爆炸穿透器使撞击体解体并产生碎片云。然而,现有的缓解分析往往忽略了轨道动力学对碎片轨迹的影响。目的:我们旨在研究撞击体碎片云的轨道动力学对不同拦截日期下撞击地球碎片数量的影响,并探讨自引力凝聚及撞击体轴向自转的作用。方法:我们使用运行于GPU上的八阶高精度直接N体积分器计算了10^5个碎片的轨道,考虑了太阳系中所有大天体的轨道摄动以及碎片云的自引力。结果:通过一系列数值实验,我们表明轨道剪切导致碎片云呈三轴椭球形状。三轴椭球的形状和取向受到碎片云轨道轨迹的强烈调制,进而影响碎片云相对于地球的撞击截面。因此,撞击地球的碎片数量受到撞击体轨道和拦截时间的强烈影响。对于明确的撞击体自转轴取向,撞击次数达到最小值,该取向取决于拦截日期。结论:为最小化PHA撞击的致命后果,需要精确约束拦截时机。对于阿波罗型或阿登型PHA,过早拦截可能并非理想选择。因此,我们发现拦截PHA的最佳时机是其运行至轨道近心点时。

英文摘要:

Context: Potentially hazardous asteroids (PHA) in Earth-crossing orbits pose a constant threat to life on Earth. Several mitigation methods have been proposed, and the most feasible technique appears to be the disintegration of the impactor and the generation of a fragment cloud by explosive penetrators at interception. However, mitigation analyses tend to neglect the effect of orbital dynamics on the trajectory of fragments. Aims: We aim to study the effect of orbital dynamics of the impactor's cloud on the number of fragments that hit the Earth, assuming different interception dates. We investigate the effect of self-gravitational cohesion and the axial rotation of the impactor. Methods: We computed the orbits of 10^5 fragments with a high-precision direct N-body integrator of the eighth order, running on GPUs. We considered orbital perturbations from all large bodies in the Solar System and the self-gravity of the cloud fragments. Results: Using a series of numerical experiments, we show that orbital shear causes the fragment cloud to adopt the shape of a triaxial ellipsoid. The shape and alignment of the triaxial ellipsoid are strongly modulated by the cloud's orbital trajectory and, hence, the impact cross-section of the cloud with respect to the Earth. Therefore, the number of fragments hitting the Earth is strongly influenced by the orbit of the impactor and the time of interception. A minimum number of impacts occur for a well-defined orientation of the impactor rotational axis, depending on the date of interception. Conclusions: To minimise the lethal consequences of an PHA's impact, a well-constrained interception timing is necessary. A too-early interception may not be ideal for PHAs in the Apollo or Aten groups. Thus, we find that the best time to intercept PHA is when it is at the pericentre of its orbit.

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