Feasibility of Detecting Spacecraft Charging and Arcing by Remote Sensing

被引:19
|
作者
Ferguson, Dale C. [1 ]
Murray-Krezan, Jeremy [2 ]
Barton, David A. [3 ]
Dennison, J. R. [4 ]
Gregory, Stephen A. [5 ]
机构
[1] US Air Force Res Lab, Space Vehicles Directorate, RVBXR, Kirtland AFB, NM 87117 USA
[2] US Air Force Res Lab, Space Vehicles Directorate, RVSV, Adv Res Collaborat & Dev Environm ARCADE, Kirtland AFB, NM 87117 USA
[3] US Air Force Res Lab, Space Vehicles Directorate, RVBXR, Calibrat & Test Chamber Electron Radiat CaTChER, Kirtland AFB, NM 87117 USA
[4] Utah State Univ, Dept Phys, Mat Phys Grp, Logan, UT 84322 USA
[5] Boeing LTS Inc, Kirtland AFB, NM 87117 USA
关键词
D O I
10.2514/1.A32958
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
More than 50 years after the dawn of the space age, most spacecraft still do not have sensors onboard capable of detecting whether they are at potentials likely to put them at risk of severe charging and the concomitant arcing, or, indeed, even capable of detecting when or if they undergo arcing. As a result, anomaly resolution has often been hit or miss, and false diagnoses are probably common. In this paper, a few remote sensing techniques that could be applied for remotely detecting spacecraft charging and/or arcing, and their feasibility, are examined: surface glows from high-energy electron impact, x-rays from bremsstrahlung, and radio and optical emission from arcs and after arcing.
引用
收藏
页码:1907 / 1913
页数:7
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