Spitzer Observations of Spacecraft Target 162173 (1999 JU3)
H. Campins, J. P. Emery, M. Kelley, Y. Fernandez, J. Licandro, M., Delbo, A. Barucci, E. Dotto

TL;DR
This study uses Spitzer Space Telescope mid-infrared observations to analyze the surface properties and thermal inertia of asteroid 162173 (1999 JU3), aiding future sample return missions by constraining its surface characteristics.
Contribution
It provides new thermal infrared data and models to estimate the thermal inertia of 1999 JU3, considering different spin-pole orientations, which improves understanding of its surface properties.
Findings
Thermal inertia lower limit of 150 J/m^2/K/s^0.5 for equatorial retrograde orientation.
Best-fit thermal inertia of approximately 700+/-200 J/m^2/K/s^0.5 with certain pole assumptions.
Higher thermal inertia values are possible, indicating a less fine regolith surface.
Abstract
Near-Earth asteroid 162173 (1999 JU3) is the primary target of the Hayabusa-2 sample return mission, and a potential target of the Marco Polo sample return mission. Earth-based studies of this object are fundamental to these missions. We present a mid-infrared spectrum (5-38 microns) of 1999 JU3 obtained with NASA's Spitzer Space Telescope in May 2008. 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. In the extreme case of an equatorial retrograde geometry we derive a lower limit to the thermal inertia of 150 J/m^2/K/s^0.5. If we adopt the pole…
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