Paper
16 February 2004 Self-sealing materials for space debris shield
M. Tochizawa, N. Inoue, M. Tanaka, Yoshitake Nishi
Author Affiliations +
Proceedings Volume 5648, Smart Materials III; (2004) https://doi.org/10.1117/12.582279
Event: Smart Materials, Nano-, and Micro-Smart Systems, 2004, Sydney, Australia
Abstract
To protect space structures from debris impact, the new types of shield using a self-sealing materials are suggested. A hole by debris impact on shield will be fixed with the self-sealing materials by melting, sealing and solidification. Time to seal impact hole was experimentally simulated. If time to seal impact hole was assumed to be about 5 s, viscosity of self-sealing materials should be about 0.5 Pa s. In addition, glasses with supercooled liquids at elevated temperatures were also suggested as candidate materials for sealing, because low values of viscosity were obtained below melting points. From these results, boride ceramics, high temperature polymer materials including a liquid-crystal and light metallic glasses were suggested as the candidate materials for the self-sealing system.
© (2004) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
M. Tochizawa, N. Inoue, M. Tanaka, and Yoshitake Nishi "Self-sealing materials for space debris shield", Proc. SPIE 5648, Smart Materials III, (16 February 2004); https://doi.org/10.1117/12.582279
Advertisement
Advertisement
RIGHTS & PERMISSIONS
Get copyright permission  Get copyright permission on Copyright Marketplace
KEYWORDS
Liquids

Solids

Protactinium

Crystals

Glasses

Liquid crystals

Temperature metrology

Back to Top