Electrostatic space radiation shielding

被引:23
|
作者
Tripathi, Ram K. [1 ]
Wilson, John W. [1 ]
Youngquist, Robert C. [2 ]
机构
[1] NASA, Langley Res Ctr, Hampton, VA 23681 USA
[2] NASA, John F Kennedy Space Ctr, Kennedy Space Ctr, FL 32899 USA
关键词
electrostatic space radiation shielding; active radiation shielding; radiation shielding and protection; human space missions; space radiation exposure;
D O I
10.1016/j.asr.2007.09.015
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
For the success of NASA's new vision for space exploration to Moon, Mars and beyond, exposures from the hazards of severe space radiation in deep space long duration missions is 'a must solve' problem. The payload penalty demands a very stringent requirement on the design of the spacecrafts for human deep space missions. The exploration beyond low Earth orbit (LEO) to enable routine access of space will require protection from the hazards of the accumulated exposures of space radiation, Galactic Cosmic Rays (GCR) and Solar Particle Events (SPE), and minimizing the production of secondary radiation is a great advantage. There is a need to look to new horizons for newer technologies. The present investigation revisits electrostatic active radiation shielding and explores the feasibility of using the electrostatic shielding in concert with the state-of-the-art materials shielding and protection technologies. The full space radiation environment has been used, for the first time, to explore the feasibility of electrostatic shielding. The goal is to repel enough positive charge ions so that they miss the spacecraft without attracting thermal electrons. Conclusions are drawn for the future directions of space radiation protection. Published by Elsevier Ltd. on behalf of COSPAR.
引用
收藏
页码:1043 / 1049
页数:7
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