A material’s Coefficient of Thermal Expansion (CTE) is a valuable physical property, particularly for structural fiber reinforced composites that are routinely used in satellite/aerospace applications. Satellite space structures are routinely designed with a high degree of dimensional and thermal stability. Designing and verifying for near zero CTE performance is a common design requirement. The CTE is routinely a physical property with known values for common materials. However, the strength, stiffness and CTE properties on a multi-ply graphite fiber reinforced laminate composite can be tailored to specific engineering requirements. Because of this, a method of verification (testing) is routinely performed to ensure these requirements are met.
| Identifer | oai:union.ndltd.org:lmu.edu/oai:digitalcommons.lmu.edu:etd-1326 |
| Date | 01 July 2018 |
| Creators | Uchimiya, Ronald |
| Publisher | Digital Commons at Loyola Marymount University and Loyola Law School |
| Source Sets | Loyola Marymount University |
| Detected Language | English |
| Type | text |
| Format | application/pdf |
| Source | LMU/LLS Theses and Dissertations |
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