Space environmental effects: Construction and utilization of a system to measure low thermal strain in one meter graphite epoxy tubes
Abstract
A system for measuring the expansion of low coefficient of thermal expansion (CTE) materials was constructed around a H.P. 5526-A laser measuring system. The vacuum CTE measurements in the -150 F to +120 F range were made over a 6 month period on a graphite epoxy tube yielding CTE values of 2.5 to one fifty-millionth/F above ambient and 2 + or - one ten-millionth F below ambient temperature. To assure that the below ambient, approximately 10 microns high open loop nature of the delta L/L vs. T curves was not apparatus related, similar size quartz tubes (A and B) were checked and found to have only a 2 micron (negligable for quartz) open loop component. These two quartz tubes, A and B, had ambient CTE values 20% and 45% respectively higher than the average handbook value. The overnight microcreep diminished an order of magnitude during the first several cycles after the system had been reopened.
- Publication:
-
Alabama Univ., Huntsville Report
- Pub Date:
- January 1982
- Bibcode:
- 1982alab.rept.....D
- Keywords:
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- Aerospace Environments;
- Graphite-Epoxy Composites;
- Heat Transfer Coefficients;
- Thermal Expansion;
- Thermal Stresses;
- Creep Properties;
- Hubble Space Telescope;
- Quartz;
- Temperature Gradients;
- Instrumentation and Photography