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Analytical formulation of lunar cratering asymmetries

机译:月球陨石坑不对称的解析公式

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Context. The cratering asymmetry of a bombarded satellite is related to both its orbit and impactors. The inner solar system impactor populations, that is, the main-belt asteroids (MBAs) and the near-Earth objects (NEOs), have dominated during the late heavy bombardment (LHB) and ever since, respectively. Aims. We formulate the lunar cratering distribution and verify the cratering asymmetries generated by the MBAs as well as the NEOs. Methods. Based on a planar model that excludes the terrestrial and lunar gravitations on the impactors and assuming the impactor encounter speed with Earth venc is higher than the lunar orbital speed vM, we rigorously integrated the lunar cratering distribution, and derived its approximation to the first order of vM/venc. Numerical simulations of lunar bombardment by the MBAs during the LHB were performed with an Earth–Moon distance aM = 20?60 Earth radii in five cases. Results. The analytical model directly proves the existence of a leading/trailing asymmetry and the absence of near/far asymmetry. The approximate form of the leading/trailing asymmetry is (1 + A1cosβ), which decreases as the apex distance β increases. The numerical simulations show evidence of a pole/equator asymmetry as well as the leading/trailing asymmetry, and the former is empirically described as (1 + A2cos2?), which decreases as the latitude modulus | ? | increases. The amplitudes A1,2 are reliable measurements of asymmetries. Our analysis explicitly indicates the quantitative relations between cratering distribution and bombardment conditions (impactor properties and the lunar orbital status) like A1 ∝ vM/venc, resulting in a method for reproducing the bombardment conditions through measuring the asymmetry. Mutual confirmation between analytical model and numerical simulations is found in terms of the cratering distribution and its variation with aM. Estimates of A1 for crater density distributions generated by the MBAs and the NEOs are 0.101?0.159 and 0.117, respectively.
机译:上下文。轰炸卫星的陨石坑不对称性与其轨道和撞击器有关。在重磅炸弹轰炸后期(LHB)期间以及此后,太阳系内部撞击者种群(即主要的小行星小行星(MBA)和近地天体(NEO))分别占主导地位。目的我们制定月球陨石坑分布并验证由MBA和NEO产生的陨石坑不对称性。方法。基于一个平面模型,该模型排除了撞击者的地心引力和月球引力,并假设撞击者与地球venc的接触速度高于月球轨道速度vM,我们严格地综合了月球陨石坑分布,并将其近似推导为vM / venc。在5个案例中,LHB期间MBA轰炸月球的数值模拟是通过地月距离aM = 20?60地球半径进行的。结果。分析模型直接证明了前/后不对称性的存在以及近/远不对称性的存在。前/后不对称的近似形式为(1 +A1cosβ),其随着顶点距离β的增加而减小。数值模拟显示了极/赤道不对称以及超前/后向不对称的证据,根据经验,前者描述为(1 + A2cos2?),随着纬度模数| ? |增加。幅度A1,2是不对称性的可靠测量。我们的分析明确指出了缩孔分布与轰击条件(撞击物性质和月球轨道状态)之间的定量关系,如A1 ∝ vM / venc,从而产生了一种通过测量不对称性来再现轰击条件的方法。根据缩孔分布及其随aM的变化,发现了分析模型与数值模拟之间的相互确认。 MBA和NEO产生的火山口密度分布的A1估计分别为0.101-0.159和0.117。

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