Auroral particle instrument onboard the index satellite

被引:42
作者
Asamura, K
Tsujita, D
Tanaka, H
Saito, Y
Mukai, T
Hirahara, M
机构
[1] Inst Space & Astronaut Sci, Sagamihara, Kanagawa 2298510, Japan
[2] Rikkyo Univ, Fac Sci, Tokyo 1718501, Japan
来源
FUTURE TRENDS AND NEEDS IN SCIENCE AND ENGINEERING FOR PLASMA PHYSICS IN SPACE | 2003年 / 32卷 / 03期
关键词
D O I
10.1016/S0273-1177(03)90275-4
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The INDEX satellite is a microsatellite which will be inserted into a low-altitude (680 km) polar orbit. A low-energy plasma particle instrument, which consists of two sensor heads (electron/ions sensors; ESA/ISA) and a multi-spectral auroral camera (MAC) will be installed in the INDEX - satellite in order to investigate formation mechanisms of fine-scale structures of optical auroral arc emissions. One of advantages of the INDEX mission is that the satellite is capable to observe fine-scale auroral arc emissions and corresponding auroral particles simultaneously by controlling an attitude of the satellite. Since the satellite velocity is relatively fast, a high time-resolution is necessary for the plasma measurement. The time resolution of the plasma instruments onboard the INDEX satellite is 20 ms, which corresponds to a spatial scale of similar to150m. (C) 2003 COSPAR. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:375 / 378
页数:4
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