SpaceSkin - development of aerospace-grade electronic textile for simultaneous protection and high velocity impact characterization

被引:12
作者
Cherston, Juliana [1 ]
Paradiso, Joseph A. [1 ]
机构
[1] MIT, Media Lab Respons Environm Grp, 75 Amherst St, Cambridge, MA 02139 USA
来源
SENSORS AND SMART STRUCTURES TECHNOLOGIES FOR CIVIL, MECHANICAL, AND AEROSPACE SYSTEMS 2019 | 2019年 / 10970卷
关键词
electronic textiles; aerospace skin; damage detection; smart fabrics; smart fibers; multifunctional systems; aerospace materials; space structures; PLASMA; DESIGN;
D O I
10.1117/12.2513962
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
This paper introduces the concept of an aerospace-grade electronic textile and summarizes design studies and early prototype development for on-fabric hypervelocity impact characterization. Whereas most damage detection technologies for aerospace systems rely on enhancements to the structure's inner shell, the outermost protective skin of a space habitat or a spacesuit - traditionally a woven fabric - is directly exposed to the relevant environment. Therefore, we propose weaving sensory fibers into traditional fibrous aerospace skins for direct measurement of local conditions, yielding a material that can simultaneously sense and protect. Specifically, this paper documents design considerations for multifunctional Beta cloth, in which piezoelectric yarn is directly woven into Teflon-coated fiberglass, the material used as the outermost skin of the International Space Station. A review of hypervelocity plasma generation then motivates a strawman design for on-textile plasma charge and RF emission sensing, which may be useful for further characterization of hypervelocity impactors. An aerospace-grade electronic textile is distinct from a traditional e-textile in that it must be validated not only for its sensing capabilities but also for its robustness to hazards presented in a space environment.
引用
收藏
页数:15
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