Thermal expansion of graphite-epoxy between 116 K and 366 K
Abstract
A Priest laser interferometer was developed to measure the thermal strain of composite laminates. The salient features of this interferometer are that: (1) it operates between 116 K and 366 K; (2) it is easy to operate; (3) minimum specimen preparation is required; (4) coefficients of thermal expansion in the range of 0-5 micro epsilon/K can be measured; and (5) the resolution of thermal strain is on the order of micro epsilon. The thermal response of quasi-isotropic, T300/5208, grahite-epoxy composite material was studied with this interferometer. The study showed that: (1) for the material tested, thermal cycling effects are negligible; (2) variability of thermal response from specimen to specimen may become significant at cryogenic temperatures; and (3) the thermal response of 0.6 cm and 2.5 cm wide specimens are the same above room temperature.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- March 1982
- Bibcode:
- 1982STIN...8218280S
- Keywords:
-
- Graphite-Epoxy Composites;
- Large Space Structures;
- Thermal Cycling Tests;
- Thermal Expansion;
- Thermal Stresses;
- Equipment Specifications;
- Interferometers;
- Mechanical Properties;
- Molybdenum;
- Temperature Dependence;
- Thermodynamics;
- Launch Vehicles and Space Vehicles