A ground-based observation of the LCROSS impact events using the Subaru Telescope

► We conducted infrared spectral and imaging observations of the LCROSS impacts using the Subaru Telescope. ► No unambiguous emission line of H 2O or dust was detected. ► The upper limit for dust mass was significantly smaller than that predicted by a standard impact theory. ► The cratering process...

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Veröffentlicht in:Icarus (New York, N.Y. 1962) N.Y. 1962), 2011-07, Vol.214 (1), p.21-29
Hauptverfasser: Hong, Peng K., Sugita, Seiji, Okamura, Natsuko, Sekine, Yasuhito, Terada, Hiroshi, Takatoh, Naruhisa, Hayano, Yutaka, Fuse, Tetsuharu, Pyo, Tae-Soo, Kawakita, Hideyo, Wooden, Diane H., Young, Eliot F., Lucey, Paul G., Kurosawa, Kosuke, Genda, Hidenori, Haruyama, Junichi, Furusho, Reiko, Kadono, Toshihiko, Nakamura, Ryosuke, Kamata, Shunichi, Hamura, Taiga, Sekiguchi, Tomohiko, Sôma, Mitsuru, Noda, Hirotomo, Watanabe, Jun-ichi
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Sprache:eng
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Zusammenfassung:► We conducted infrared spectral and imaging observations of the LCROSS impacts using the Subaru Telescope. ► No unambiguous emission line of H 2O or dust was detected. ► The upper limit for dust mass was significantly smaller than that predicted by a standard impact theory. ► The cratering process may have been greatly different from the standard cratering theory possibly because of its hollow projectile structure. The Lunar Crater Observation and Sensing Satellite (LCROSS) mission was an impact exploration searching for a volatile deposit in a permanently shadowed region (PSR) by excavating near-surface material. We conducted infrared spectral and imaging observations of the LCROSS impacts from 15 min before the first collision through 2 min after the second collision using the Subaru Telescope in order to measure ejecta dust and water. Such a ground-based observation is important because the viewing geometry and wavelength coverage are very different from the LCROSS spacecraft. We used the Echelle spectrograph with spectral resolution λ/Δ λ ∼ 10,000 to observe the non-resonant H 2O rotational emission lines near 2.9 μm and the slit viewer with a K′ filter for imaging observation of ejecta plumes. Pre-impact calculations using a homogeneous projectile predicted that 2000 kg of ejecta and 10 kg of H 2O were excavated and thrown into the analyzed area immediately above the slit within the field of view (FOV) of the K′ imager and the FOV of spectrometer slit, respectively. However, no unambiguous emission line of H 2O or dust was detected. The estimated upper limits of the amount of dust and H 2O from the main Centaur impact were 800 kg and 40 kg for the 3 σ of noise in the analyzed area within the imager FOV and in the slit FOV, respectively. If we take 1 σ as detection limit, the upper limits are 300 kg and 14 kg, respectively. Although the upper limit for water mass is comparable to a prediction by a standard theoretical prediction, that for dust mass is significantly smaller than that predicted by a standard impact theory. This discrepancy in ejecta dust mass between a theoretical prediction and our observation result suggests that the cratering process induced by the LCROSS impacts may have been substantially different from the standard cratering theory, possibly because of its hollow projectile structure.
ISSN:0019-1035
1090-2643
DOI:10.1016/j.icarus.2011.05.008