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The origin of Phobos grooves from ejecta launched from impact craters on Mars: Tests of the hypothesis

机译:火星上火星撞击坑发射的喷出物的火卫一沟槽的起源:假设检验

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The surface of the martian moon Phobos is characterized by parallel and intersecting grooves that bear resemblance to secondary crater chains observed on planetary surfaces. Murray (2011) has hypothesized that the main groove-forming process on Phobos is the intersection of Phobos with ejecta from primary impact events on Mars to produce chains of secondary craters. The hypothesis infers a pattern of parallel jets of ejecta, either fluidized or solidified, that break into equally-spaced fragments and disperse uniformly along-trajectory during the flight from Mars to Phobos. At the moment of impact with Phobos the dispersed fragments emplace secondary craters that are aligned along strike corresponding to the flight pattern of ejecta along trajectory. The aspects of the characteristics of grooves on Phobos cited by this hypothesis that might be explained by secondary ejecta include: their observed linearity, parallelism, planar alignment, pitted nature, change in character along strike, and a "zone of avoidance" where ejecta from Mars is predicted not to impact (Murray, 2011). To test the hypothesis we plot precise Keplerian orbits for ejecta from Mars (elliptical and hyperbolic with periapsis located below the surface of Mars). From these trajectories we: (1) set the fragment dispersion limits of ejecta patterns required to emplace the more typically well-organized parallel grooves observed in returned images from Phobos; (2) plot ranges of the ejecta flight durations from Mars to Phobos and map regions of exposure; (3) utilize the same exposure map to observe trajectory-defined ejecta exposure shadows; (4) observe hemispheric exposure in response to shorter and longer durations of ejecta flight; (5) assess the viability of ejecta emplacing the large family of grooves covering most of the northern hemisphere of Phobos; and (6) plot the arrival of parallel lines of ejecta emplacing chains of craters at oblique incident angles. We also assess the bulk volume of ejecta from martian impact events and the number of events that are necessary to supply sufficient bulk densities of secondary impactor fragments. On the basis of our analysis, we find that six major predictions of the Murray hypothesis are not consistent with a wide range of Mars ejecta emplacement models and observations as follows: (1) To emplace families of parallel grooves as observed in the most common features (grooves that manifest virtually no positional defects), and to reach the maximum geographic extent of Phobos, grid patterns of ejecta fragments must be produced with nearly identical diameters (often tens of thousands in number) and must launch with virtually zero rates of dispersion (<1 mm/s and <1.0|irad in all degrees of freedom) into fixed patterns of arrays where fragment dispersion is referenced to a common datum point for the duration of flights from Mars to Phobos of up to 3 h. (2) Half of the areal region observed as a "zone of avoidance" (where grooves are absent on the trailing orbital apex of Phobos) is directly exposed to ejecta trajectories from the surface of Mars, which suggests that the "zone of avoidance" is unrelated to ejecta trajectories. (3) Several families of grooves display groove segments that are observed in a region of Phobos that is shadowed from martian ejecta trajectories for flight durations up to 3 h. Where the Murray hypothesis predicts the emplacement of groove families from a single ejecta plume, this strongly suggests that these families of grooves could not have been produced by martian impact ejecta. (4) To reach increasingly westerly locations of Phobos ejecta must travel in space for substantially longer flight times (up to 20X) which would produce substantially lower secondary crater densities on the anti-Mars side of Phobos and observably reduce their pit organization. This is not observed. (5) The largest family of grooves cannot be emplaced by any valid trajectory from Mars in its present day or ancient orbit. (6) If emplaced by grid patterns of ejecta, the irregular topography and small-body radius of Phobos would clearly disrupt groove family linearity and parallelism due to the preponderance of oblique incident angle impacts. However, when viewed from any position, the vast majority of groove families and individual grooves appear to completely avoid the effects of Phobos' morphology. Based on our analysis we conclude that the Murray hypothesis, that many Phobos grooves are formed by intersection of ejecta from craters on Mars, is not valid.
机译:火星卫星火卫一的表面特征是平行且相交的凹槽,与行星表面观察到的第二弹坑链相似。 Murray(2011)假设,火卫一上的主要沟纹形成过程是火卫一与火星上一次撞击事件的喷出物相交,形成第二个陨石坑链的交集。该假设推断出流化或凝固的平行喷射射流的模式,在从火星飞往火卫一的过程中,它们分裂成等距的碎片并沿轨迹均匀分散。在与火卫一撞击的时刻,分散的碎片会形成次级弹坑,这些弹坑沿着与射弹沿着轨迹的飞行模式相对应的走向对齐。该假设所引用的Phobos上凹槽的特性方面可能由次生喷射来解释,这些方面包括:观测到的线性,平行度,平面对齐,凹痕性质,沿击打的特征变化以及“喷射回避”区域预计火星不会产生影响(Murray,2011年)。为了检验该假设,我们绘制了火星喷射的精确开普勒轨道(椭圆形和双曲线,并在火星表面以下有围ap)。从这些轨迹中,我们:(1)设置喷射位置的碎片散布极限,以放置从火卫一返回的图像中观察到的更为典型的组织良好的平行凹槽; (2)绘制从火星到火卫一的射出飞行持续时间的范围,并绘制暴露区域图; (3)利用相同的曝光图来观察轨迹定义的喷射曝光阴影; (4)观察半球暴露,以响应越来越短的喷射飞行时间; (5)评估喷射器的可行性,该喷射器包括覆盖火卫一北半球大部分地区的大型沟纹; (6)画出了在倾斜入射角处包围弹坑的弹射链的平行线的到达。我们还评估了来自火星撞击事件的排出物的总体积,以及提供足够的第二撞击物碎片体积密度所必需的事件数量。根据我们的分析,我们发现,关于Murray假说的六个主要预测与以下各种Marsjecta进位模型和观测结果不一致:(1)放置在最常见特征中观察到的平行沟槽族(实际上没有任何位置缺陷的凹槽),并且要达到Phobos的最大地理范围,必须以几乎相同的直径(通常为数万个)制作出喷射碎片的网格图案,并且必须以几乎为零的分散速率发射(小于1mm / s,并且在所有自由度上均小于<1.0 | irad)形成固定的阵列阵列,其中碎片散布以从火星到火卫一的飞行长达3小时的时间指向一个共同的基准点。 (2)被观察为“避让区”的区域区域(火卫一的后轨道顶点上没有凹槽)直接暴露于火星表面的弹射轨迹,这表明“避让区”与弹射轨迹无关。 (3)几个系列的凹槽显示了在火卫一的区域内观察到的凹槽段,该区域被火星喷射轨迹遮挡了长达3小时的飞行时间。在Murray假设从单个喷射射流羽预测凹槽族的位置的情况下,这强烈表明这些火星族不可能由火星撞击喷射产生。 (4)为了到达火星上越来越西风的位置,必须在太空中飞行更长的飞行时间(最多20倍),这将在火卫一的反火星一侧产生次要的陨石坑密度,并明显减少其坑坑结构。这没有被观察到。 (5)最大的凹槽族不能被火星在其现今或古代轨道上的任何有效轨迹所占据。 (6)如果被喷射的网格状图案所包围,由于斜入射角的影响,火卫一的不规则形貌和小体半径显然会破坏沟槽族的线性和平行度。但是,从任何位置看,绝大多数凹槽族和单个凹槽似乎完全避免了Phobos形态的影响。根据我们的分析,我们得出的结论是,Murray假说是无效的,该假说认为许多Phobos凹槽是由火星陨石坑的弹射相交形成的。

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