Design of electrostatic accelerators for the development of microparticle detectors in Japan

被引:7
作者
Hasegawa, S [1 ]
Fujiwara, A
Yano, H
Nisimura, T
Sasaki, S
Ohashi, H
Iwai, T
Kobayashi, K
Shibata, H
机构
[1] Inst Space & Astronaut Sci, Res Div Planetary Sci, Kanagawa 229, Japan
[2] NASA, Lyndon B Johnson Space Ctr, Earth Sci & Solar Syst Explorat Div, Houston, TX 77058 USA
[3] Inst Phys & Chem Res, Atom Phys Lab, Saitama, Japan
[4] Univ Tokyo, Dept Geol, Tokyo, Japan
[5] Tokyo Univ Fisheries, Dept Ocean Sci, Tokyo 108, Japan
[6] Univ Tokyo, Nucl Sci & Technol Res Ctr, Tokyo 113, Japan
来源
SPACE DEBRIS | 1999年 / 23卷 / 01期
关键词
D O I
10.1016/S0273-1177(98)00238-5
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Micrometeoroid detection in space usually involves high-velocity impact phenomena. In-situ dust detectors should be calibrated by a microparticle accelerator with a mass and velocity range comparable to micrometeoroids. A pilot model of an accelerator was constructed some years ago and fundamental research for an advanced facility has been performed. We are developing two new accelerators. A 3.75MV Van de Graaff electrostatic accelerator at The Research Center for Nuclear Science and Technology, University of Tokyo, has been modified to accelerate microparticles, and acceleration testing is now being carried but. The expected velocity range is 1-20 km/s for micron or sub-micron particles. Another small accelerator will be installed for easier handling, more frequent use, and lower-cost operation. (C) 1999 COSPAR. Published by Elsevier Science Ltd.
引用
收藏
页码:119 / 122
页数:4
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