JpGU-AGU Joint Meeting 2020

講演情報

[E] ポスター発表

セッション記号 P (宇宙惑星科学) » P-PS 惑星科学

[P-PS01] Outer Solar System Exploration Today, and Tomorrow

コンビーナ:木村 淳(大阪大学)、Kunio M. Sayanagi(Hampton University)、土屋 史紀(東北大学大学院理学研究科惑星プラズマ・大気研究センター)、Steven Douglas Vance(NASA Jet Propulsion Laboratory, California Institute of Technology)

[PPS01-P07] Detectability of water plumes on icy moons with Earth-orbiting UV telescope

*古賀 亮一1土屋 史紀1村上 豪3吉岡 和夫2鍵谷 将人1木村 智樹1山崎 敦3吉川 一朗2北 元3桑原 正輝3 (1.東北大学、2.東京大学、3.宇宙科学研究所)

In this study, we consider the mirror size of UV space telescope, which can detect OI and HI emissions emitted from plumes on icy moons. Hubble Space Telescope (HST) observed the enhancement of HI 121.6 nm and OI 130.4 nm emissions near the Europa South Pole (Roth et al., 2014). They considered the electron impact of H2O in the plume yields HI and OI emissions. However, geological conditions of emitting gasses form Europa plumes are not known.

The EXCEED (Extreme Ultraviolet Spectroscope for Exospheric Dynamics) spectrometer onboard the Hisaki satellite has conducted long term monitoring of ultraviolet emissions (52.0-148.0 nm) from the Io plasma torus and Jupiter’s aurora since 2013. We also observed OI 130.4 nm around Jupiter moon Io’s orbit, and analyzed spatial distribution and temporal variations of oxygen atoms in Io torus. However, the spatial resolution of Hisaki/EXCEED is too rough (~17”) to resolve Io and Icy moon’s disk (for example, Europa’s diameter is ~1.0”). One of the main goal of post Hisaki UV satellite is to observe icy moon’s atmosphere continuously with high resolution and confine conditions under which plume eruptions occur.

We calculated the OI 130.4 nm and HI 121.6 nm counts of Europa plume (signal) and atmosphere, solar reflection, geocorona and interplanetary medium (noise), and estimated the mirror diameters, which can meet the demand that the signal to noise ratio is over 3 with integration time of 10 hours and spatial resolution of ~0.2 arcsec. Requested mirror diameters are ~140 cm when the altitude of the satellite is 1000 km, and ~100 cm when the altitude is 30,000 km.