The space environment is quite hostile to structural materials. The lifetime of space-craft is determined by the environmentally induced degradation of the structural materials. The self-healing systems discussed in this book chapter are applied mainly to polymer matrix-based materials. They usually include a variety of epoxies, polyimides, polysulfones and phenolics. In particular, cyanate-ester resins have been considered due to their lower hygrostrain/outgassing compared to the first generation of epoxy matrices. Carbon, glass and aramid fibres have also been used as reinforcing filaments within composite space structures. Aramid fibres are often employed as a `buffer' within a shielding system against damage induced by micrometeoroid impacts.
Self-healing in space environment, Page 1 of 2
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