TY - JOUR
T1 - Low-energy charged particle measurement by MAP-PACE onboard SELENE
AU - Saito, Yoshifumi
AU - Yokota, Shoichiro
AU - Asamura, Kazushi
AU - Tanaka, Takaaki
AU - Akiba, Ryota
AU - Fujimoto, Masaki
AU - Hasegawa, Hiroshi
AU - Hayakawa, Hajime
AU - Hirahara, Masafumi
AU - Hoshino, Masahiro
AU - Machida, Shinobu
AU - Mukai, Toshifumi
AU - Nagai, Tsugunobu
AU - Nagatsuma, Tsutomu
AU - Nakamura, Masato
AU - Oyama, Koh ichiro
AU - Sagawa, Eiichi
AU - Sasaki, Susumu
AU - Seki, Kanako
AU - Terasawa, Toshio
PY - 2008
Y1 - 2008
N2 - MAP-PACE (MAgnetic field and Plasma experiment-Plasma energy Angle and Compostion Experiment) is one of the scientific instruments onboard the SELENE (SELenological and ENgineering Explorer) satellite. PACE consists of four sensors: ESA (Electron Spectrum Analyzer)-S1, ESA-S2, IMA (Ion Mass Analyzer), and IEA (Ion Energy Analyzer). ESA-S1 and S2 measure the distribution function of low-energy electrons below 15 keV, while IMA and IEA measure the distribution function of low energy ions below 28 keV/q. Each sensor has a hemispherical field of view. Since SELENE is a three-axis stabilized spacecraft, a pair of electron sensors (ESA-S1 and S2) and a pair of ion sensors (IMA and IEA) are necessary for obtaining a three-dimensional distribution function of electrons and ions. The scientific objectives of PACE are (1) to measure the ions sputtered from the lunar surface and the lunar atmosphere, (2) to measure the magnetic anomaly on the lunar surface using two ESAs and a magnetometer onboard SELENE simultaneously as an electron reflectometer, (3) to resolve the Moon-solar wind interaction, (4) to resolve the Moon-Earth's magnetosphere interaction, and (5) to observe the Earth's magnetotail.
AB - MAP-PACE (MAgnetic field and Plasma experiment-Plasma energy Angle and Compostion Experiment) is one of the scientific instruments onboard the SELENE (SELenological and ENgineering Explorer) satellite. PACE consists of four sensors: ESA (Electron Spectrum Analyzer)-S1, ESA-S2, IMA (Ion Mass Analyzer), and IEA (Ion Energy Analyzer). ESA-S1 and S2 measure the distribution function of low-energy electrons below 15 keV, while IMA and IEA measure the distribution function of low energy ions below 28 keV/q. Each sensor has a hemispherical field of view. Since SELENE is a three-axis stabilized spacecraft, a pair of electron sensors (ESA-S1 and S2) and a pair of ion sensors (IMA and IEA) are necessary for obtaining a three-dimensional distribution function of electrons and ions. The scientific objectives of PACE are (1) to measure the ions sputtered from the lunar surface and the lunar atmosphere, (2) to measure the magnetic anomaly on the lunar surface using two ESAs and a magnetometer onboard SELENE simultaneously as an electron reflectometer, (3) to resolve the Moon-solar wind interaction, (4) to resolve the Moon-Earth's magnetosphere interaction, and (5) to observe the Earth's magnetotail.
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U2 - 10.1186/BF03352802
DO - 10.1186/BF03352802
M3 - Article
AN - SCOPUS:46849086163
SN - 1343-8832
VL - 60
SP - 375
EP - 385
JO - Earth, Planets and Space
JF - Earth, Planets and Space
IS - 4
ER -