Thermal expansion of composites: Methods and results
Abstract
The factors controlling the dimensional stability of various components of large space structures were investigated. Cyclic, thermal and mechanical loading were identified as the primary controlling factors of the dimensional stability of cables. For organic matrix composites, such as graphite-epoxy, it was found that these factors include moisture desorption in the space environment, thermal expansion as the structure moves from the sunlight to shadow in its orbit, mechanical loading, and microyielding of the material caused by microcracking of the matrix material. The major focus was placed on the thermal expansion of composites and in particular the development and testing of a method for its measurement.
- Publication:
-
Large Space Systems Technology, 1980
- Pub Date:
- February 1981
- Bibcode:
- 1981lsst....1..119B
- Keywords:
-
- Graphite-Epoxy Composites;
- Large Space Structures;
- Thermal Expansion;
- Electrical Resistance;
- High Temperature;
- Strain Gages;
- Launch Vehicles and Space Vehicles