Published April 2013
| Version v1
Publication
Searching the pole solution of NEA 162173 (1999 JU3)
Contributors
Others:
- Department of Astronomy ; Yonsei University
- Korea Astronomy and Space Science Institute (KASI)
- Astronomical Institute of Charles University ; Charles University [Prague] (CU)
- Department of Physics and Astronomy [Seoul] ; Seoul National University [Seoul] (SNU)
- Max-Planck-Institut für Extraterrestrische Physik (MPE)
- Okayama Astrophysical Observatory ; National Astronomical Observatory of Japan (NAOJ)
- Institute of Space and Astronautical Science (ISAS) ; Japan Aerospace Exploration Agency [Sagamihara] (JAXA)
- UNS-CNRS-Observatoire de la Côte d'Azur ; UNS-CNRS-Observatoire de la Côte d'Azur
- Institut de Mécanique Céleste et de Calcul des Ephémérides (IMCCE) ; Université Pierre et Marie Curie - Paris 6 (UPMC)-Institut national des sciences de l'Univers (INSU - CNRS)-Observatoire de Paris ; Université Paris sciences et lettres (PSL)-Université Paris sciences et lettres (PSL)-Université de Lille-Centre National de la Recherche Scientifique (CNRS)
Description
Near-Earth asteroid (NEA) 162173 (1999 JU3) (hereafter 1999 JU3) is the primary target of JAXA's Hayabusa 2 mission and also a backup target of NASA's OSIRIS-REx mission, not only because of its accessibility but also because it would be the first C-type asteroid for exploration missions. Knowing the information about spin status, such as rotational period, the ecliptic longitude and latitude of the pole is essential for the design of mission sequence such as the remote sensing observation. In order to get the physical properties of 1999 JU3, a total of 75 days ground-based observations at various geometries were carried out during 2007 - 2012 apparitions. Observations in the thermal infrared were also conducted with the Subaru, Akari, and Spitzer telescopes. We have analyzed the optical lightcurve of 1999 JU3, and derived a sidereal rotational period of 7.631 ± 0.001 hour. Using the lightcurve inversion method in conjunction with the thermal physical modeling, we determined a nearly spherical shape with a diameter of 823 ± 38 m, a geometric albedo of 0.058 ± 0.003, and a thermal inertia of 231 ± 76 J m-2 s-0.5 K-1. Although the pole orientation of 1999 JU3 is not strongly constrained, the best solution we derived is within 30 degree of (103,-20) in the ecliptic reference frame.
Abstract
Conference at the Korean Space Science Society, April 24-26 2013, Jeju island, KoreaAdditional details
Identifiers
- URL
- https://hal.sorbonne-universite.fr/hal-00821101
- URN
- urn:oai:HAL:hal-00821101v1