Aging of Polymeric Materials for Use on HSCT

942162

10/01/1994

Authors
Abstract
Content
Future commercial supersonic aircraft require long term durability of polymeric materials in environments that include temperature, fluids, loads and cyclic responses. Candidate materials studied to date indicate chemical and physical stability of composites and adhesives over long periods of time in the required thermal environment are in question. Both thermoplastic and thermoset materials show changes in mechanical performance such as open hole compression and compression after impact when exposed to isothermal environments of 177°C to 204°C beyond 5,000 hours.
Meta TagsDetails
DOI
https://doi.org/10.4271/942162
Pages
8
Citation
Rogalski, M., "Aging of Polymeric Materials for Use on HSCT," SAE Technical Paper 942162, 1994, https://doi.org/10.4271/942162.
Additional Details
Publisher
Published
Oct 1, 1994
Product Code
942162
Content Type
Technical Paper
Language
English