Space radiation transport properties of polyethylene-based composites

被引:14
作者
Kaul, RK [1 ]
Barghouty, AF
Dahche, HM
机构
[1] NASA, George C Marshall Space Flight Ctr, SD46, Huntsville, AL 35812 USA
[2] Roanoke Coll, Dept Chem, Salem, VA 24153 USA
来源
TRANSPORT PHENOMENA IN MICROGRAVITY | 2004年 / 1027卷
关键词
ionizing radiation; space radiation; shielding; shielding effectiveness; HZE; transport; simulation; transmission; polyethylene; hybrid materials; polyethylene-based composites; composites; galactic cosmic rays; solar energetic particles; deep-space missions; micrometeorite shields; Mars missions; multi-functional materials; fluences; dose; dose-equivalent; linear energy transfer;
D O I
10.1196/annals.1324.013
中图分类号
Q6 [生物物理学];
学科分类号
071011 ;
摘要
Composite materials that can serve as both effective shielding materials against cosmic-ray and energetic solar particles in deep space, as well as structural materials for habitat and spacecraft, remain a critical and mission enabling component in mission planning and exploration. Polyethylene is known to have excellent shielding properties due to its low density, coupled with high hydrogen content. Polyethylene-fiber reinforced composites promise to combine this shielding effectiveness with the required mechanical properties of structural materials. Samples of polyethylene-fiber reinforced epoxy matrix composite 1-5cm thick Were prepared at the NASA Marshall Space Flight Center and tested against a 500 MeV/nucleon Fe beam at the HIMAC facility of NIRS in Chiba, Japan. This paper presents measured and calculated results for the radiation transport properties of these samples.
引用
收藏
页码:138 / 149
页数:12
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