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首页> 外文期刊>Astronomy and astrophysics >Spitzer observations of spacecraft target 162173 (1999 JU3)
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Spitzer observations of spacecraft target 162173 (1999 JU3)

机译:斯皮策观察到的航天器目标162173(1999年3月3日)

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Context. Near-Earth asteroid 162173 (1999JU3) is the primary target of the Japanese Aerospace Exploration Agency (JAXA) Hayabusa-2 sample return mission, and is also on the list of potential targets for the European Space Agency(ESA) Marco Polo sample return mission. Earth-based studies of this object are fundamental to these missions. Aims. Our aim is to provide new constraints on the surface properties of this asteroid. Methods. We present a mid-infrared spectrum (5-38m) obtained with NASA's Spitzer Space Telescope in May 2008 and results from the application of thermal models. Results. These observations place new constraints on the surface properties of this asteroid. To fit our spectrum we used the near-Earth asteroid thermal model(NEATM) and the more complex thermophysical model(TPM). However, the position of the spin-pole, which is uncertain, is a crucial input parameter for constraining the thermal inertia with the TPM; hence, we consider two pole orientations. First is the extreme case of an equatorial retrograde geometry from which we derive a rigorous lower limit to the thermal inertia of 150Jm-2s.Second, when we adopt the pole orientation of Abe etal. (2008a, COSPAR Scientific Assembly) our best-fit thermal model yields a value for the thermal inertia of Jm-2s-0.5K-1 and even higher values are allowed by the uncertainty in the spectral shape due to the absolute flux calibration. Our best estimates of the diameter (km) and geometric albedo ()of asteroid162173 are consistent with values based on previous mid-infrared observations. Conclusions. We establish a rigorous lower limit to the thermal inertia, which is unlikely but possible, and would be consistent with a fine regolith similar to wthat is found for asteroid 433Eros. However, the thermal inertia is expected to be higher, possibly similar to or greater than that on asteroid 25143Itokawa. An Accurately determining the spin-pole of asteroid162173 will narrow the range of possible values for its thermal inertia. Key words: minor planets, asteroids - infrared: solar system - space vehicles
机译:上下文。近地小行星162173(1999JU3)是日本航空航天局(JAXA)Hayabusa-2样品返回任务的主要目标,并且还在欧洲航天局(ESA)Marco Polo样品返回任务的潜在目标之列。这些任务的地基研究是这些任务的基础。目的我们的目的是对该小行星的表面性质提供新的限制。方法。我们介绍了2008年5月用NASA的Spitzer空间望远镜获得的中红外光谱(5-38m),以及热模型的应用结果。结果。这些观察结果对该小行星的表面性质提出了新的限制。为了适应我们的光谱,我们使用了近地小行星热模型(NEATM)和更复杂的热物理模型(TPM)。然而,旋转极的位置是不确定的,它是用TPM约束热惯性的关键输入参数。因此,我们考虑两个极点方向。首先是赤道逆行几何的极端情况,从中我们得出了150Jm-2s的热惯性的严格下限。其次,当我们采用Abe等人的极方位时。 (2008a,COSPAR科学大会),我们的最佳拟合热模型得出了Jm-2s-0.5K-1的热惯性值,并且由于绝对通量校准而导致的频谱形状不确定性允许更高的值。我们对asteroid162173的直径(km)和几何反照率()的最佳估计与基于以前的中红外观测值的值一致。结论。我们为热惯性设定了一个严格的下限,这不太可能,但有可能实现,并且与类似于小行星433Eros的细粒重石相一致。但是,热惯性预计会更高,可能与小行星25143Itokawa相似或更大。准确确定asteroid162173的自旋极将缩小其热惯性的可能值范围。关键词:小行星,小行星-红外:太阳系-航天器

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