Thermal expansion behavior of LDEF metal matrix composites

T. D. Le; G. L. Steckel

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NASA NTRS · 19920018051

Thermal expansion behavior of LDEF metal matrix composites

T. D. Le·G. L. Steckel

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Abstract

The effects of the space environment on the thermal expansion stability of metal matrix composites (graphite/Al and graphite/Mg) will be presented. A sample from each category of metal matrix composites mounted on the leading and trailing edge was chosen for analysis of the temperature-time-thermal strain histories. Typical thermal expansion curves over the same range of temperature were selected at the beginning, mid, and end of the recording duration. The thermal expansion of selected post-flight LDEF samples were measured over the same range of temperature in the laboratory using a Michelson laser interferometer. The thermal strains were monitored concurrently with a laser interferometer and a mounted strain gage.

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T. D. Le, G. L. Steckel. 1992-06-01. Thermal expansion behavior of LDEF metal matrix composites. https://ntrs.nasa.gov/citations/19920018051

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