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A motivating exploration on lunar craters and low-energy dynamics in the Earth–Moon system

机译:探月系统中月球坑和低能动力学的积极探索

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It is known that most of the craters on the surface of the Moon were created by the collision of minor bodies of the Solar System. Main Belt Asteroids, which can approach the terrestrial planets as a consequence of different types of resonance, are actually the main responsible for this phenomenon. Our aim is to investigate the impact distributions on the lunar surface that low-energy dynamics can provide. As a first approximation, we exploit the hyberbolic invariant manifolds associated with the central invariant manifold around the equilibrium point L 2 of the Earth–Moon system within the framework of the Circular Restricted Three-Body Problem. Taking transit trajectories at several energy levels, we look for orbits intersecting the surface of the Moon and we attempt to define a relationship between longitude and latitude of arrival and lunar craters density. Then, we add the gravitational effect of the Sun by considering the Bicircular Restricted Four-Body Problem. In the former case, as main outcome, we observe a more relevant bombardment at the apex of the lunar surface, and a percentage of impact which is almost constant and whose value depends on the assumed Earth–Moon distance dEM. In the latter, it seems that the Earth–Moon and Earth–Moon–Sun relative distances and the initial phase of the Sun θ 0 play a crucial role on the impact distribution. The leading side focusing becomes more and more evident as dEM decreases and there seems to exist values of θ 0 more favorable to produce impacts with the Moon. Moreover, the presence of the Sun makes some trajectories to collide with the Earth. The corresponding quantity floats between 1 and 5 percent. As further exploration, we assume an uniform density of impact on the lunar surface, looking for the regions in the Earth–Moon neighbourhood these colliding trajectories have to come from. It turns out that low-energy ejecta originated from high-energy impacts are also responsible of the phenomenon we are considering.
机译:众所周知,月球表面上的大多数陨石坑是由太阳系次要物体的碰撞造成的。实际上,主带小行星由于不同类型的共振而可以接近地面行星,实际上是造成这种现象的主要原因。我们的目的是研究低能量动力学可以提供的对月球表面的影响分布。作为第一近似,我们在圆形受限三体问题的框架内,利用与地月系统平衡点L 2 周围的中心不变流形相关的双曲线不变流形。以在多个能级上的飞行轨迹,我们寻找与月球表面相交的轨道,并尝试定义经度和到达纬度与月球坑密度之间的关系。然后,我们通过考虑双圆受限四体问题来添加太阳的引力效应。在前一种情况下,作为主要结果,我们在月球表面的顶点观察到了更相关的轰炸,并且撞击的百分比几乎恒定,其值取决于假设的地球-月亮距离d EM 。在后者中,似乎地球-月亮和地球-月亮-太阳的相对距离以及太阳θ 0 的初始阶段对影响分布起着至关重要的作用。随着d EM 的减小,前端聚焦变得越来越明显,并且似乎存在更有利于与月球撞击的θ 0 值。此外,太阳的存在使一些轨迹与地球相撞。相应的数量在1-5%之间浮动。作为进一步的探索,我们假设对月球表面的撞击密度是均匀的,寻找这些碰撞轨迹必须来自地球-月球附近的区域。事实证明,源于高能冲击的低能喷射也与我们正在考虑的现象有关。

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