Thermographic monitoring of materials under simulated reentry conditionsThermography can be used to measure surface temperature gradients graphically, and can be used under conditions where the direct measurement of temperature at all desired points, using thermocouples or resistance temperature detectors (RTDs), is either difficult or impossible. The use of thermographic monitoring during a series of arc-jet tests is described. Described in this work are the issues that influence interpretation of the thermographic measurements under these conditions, including the calculation of effective emittance and window transmittance from the spectral properties of the materials in order to calculate the temperature distribution of a surface directly from the measured radiance. Comparison of the surface temperatures measured using thermocouples and the temperatures derived from thermographic measurements show good agreement. The data gathered will be used to evaluate important test parameters such as the heating distribution across the surface of a heat shield test model and at steps on the model surface.
Document ID
19910036967
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
White, Susan M. (NASA Ames Research Center Moffett Field, CA, United States)
Burleigh, Douglas (General Dynamics Corp. Space Systems Div., San Diego, CA, United States)