首页> 外文期刊>Icarus: International Journal of Solar System Studies >Orbital and thermal evolutions of four potential targets for a sample return space mission to a primitive near-Earth asteroid
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Orbital and thermal evolutions of four potential targets for a sample return space mission to a primitive near-Earth asteroid

机译:向原始近地小行星样本返回太空任务的四个潜在目标的轨道和热演化

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In this paper, we present our study of the orbital and thermal evolutions, due to solar radiative heating, of four near-Earth asteroids (NEAs) considered as potential target candidates for sample return space missions to primitive asteroids. We used a dynamical model of the NEA population to estimate the most likely source region and orbital history of these objects. Then, for each asteroid, we integrated numerically over their entire lifetime a set of 14 initially indistinguishable orbit (clones), obtained by small variations of the nominal initial conditions. Using a thermal model, we then computed surface and sub-surface temperatures of these bodies during their dynamical history. Our aim is to determine whether these bodies are likely to have experienced high temperature level, and whether great temperature changes can be expected due to the orbital changes as well as their maximum and minimum values. Such information is important in the framework of sample return space missions whose goal is to bring back pristine materials. The knowledge of the temperature range of materials at different depth over the orbital evolution of potential targets can help defining sampling strategies that ensure the likelihood that unaltered material will be brought back. Our results suggest that for all the considered potential targets, the surface has experienced for some time temperatures greater than 400. K and at most 500. K with 50% probability. This probability drops rapidly with increasing temperature. Sub-surface materials at a depth of only 3. cm are much more protected from high temperature and generally do not reach temperatures exceeding 450. K (with 50% probability). They should thus be unaltered at this depth at least from a Sun-driven heating point of view. On the other hand, surface material for some of the considered objects can have a range of temperature which can make them less reliable as pristine materials. However, it is assumed here that the same material is constantly exposed to solar heat, while regolith turnover may occur. The latter can be caused by different processes such as seismic shaking and/or impact cratering. This would reduce the total time that materials are exposed to a certain temperature. Thus, it is very likely that a sample collected from any of the four considered targets, or any primitive NEA with similar dynamical properties, will have components that will be thermally unaltered as long as some of it comes from only 3 to 5. cm depth. Such a depth is not considered difficult to reach with some of the current designs of sampling devices.
机译:在本文中,我们介绍了由于太阳辐射加热而导致的四个近地小行星(NEA)的轨道和热演化研究,这些小行星被认为是样本返回原始小行星的空间目标。我们使用了NEA种群的动力学模型来估计这些物体最可能的来源区域和轨道历史。然后,对于每个小行星,我们在其整个生命周期内通过名义初始条件的微小变化,对14个初始无法区分的轨道(克隆)进行了数值积分。然后,使用热模型,我们计算了这些物体的动力学历史过程中的表面和亚表面温度。我们的目的是确定这些物体是否可能经历了高温,以及是否可以预期由于轨道变化以及其最大值和最小值而导致温度的巨大变化。这些信息在样本回太空任务的框架中很重要,其目的是带回原始材料。在潜在目标的轨道演变过程中,不同深度的材料的温度范围的知识可帮助定义采样策略,以确保将未改变的材料带回的可能性。我们的结果表明,对于所有考虑的潜在目标,表面在一段时间内经历的温度大于400. K,最大为500. K,概率为50%。随着温度的升高,这种可能性迅速下降。深度仅为3厘米的次表层材料受到高温保护的程度更高,通常不会达到超过450. K(50%的可能性)的温度。因此,至少从太阳驱动的加热角度来看,它们应在此深度保持不变。另一方面,某些所考虑物体的表面材料可能具有一定的温度范围,这会使它们作为原始材料的可靠性降低。但是,这里假设相同的材料经常暴露在太阳热下,而可能发生碎石翻转。后者可能是由不同的过程引起的,例如地震震动和/或撞击坑。这将减少材料暴露于特定温度的总时间。因此,很可能从四个被考虑的目标中的任何一个或具有类似动态特性的任何原始NEA收集的样本,只要其中一些深度只有3至5厘米,其成分就不会发生热改变。 。当前的一些采样设备设计认为很难达到这样的深度。

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