Thomas J Horn W Lance Richards and Leslie Gong National Aeronautics and Space Administration Dryden Flight Research Center MS 48202A P O Box 273 Edwards CA 93523

Abstract:  A new open-loop heat flux control technique has been developed to conduct transient thermal testing of thick, thermallyconductive aerospace structures. This technique uses calibration of the radiant heater system power level as a function of heat flux, predicted aerodynamic heat flux, and the properties of an instrumented test article. An iterative process was used to generate open-loop heater power profiles prior to each transient thermal test. Differences between the measured and predicted surface temperatures were used to refine the heater power level command profiles through the iteration process. This iteration process has reduced the effects of environmental and test system design factors, which are normally compensated for by closed-loop temperature control, to acceptable levels. The final revised heater power profiles resulted in measured temperature time histories which deviated less than 25 ?F from the predicted surface temperatures. Keywords: structural tests, thermal testi...