Abstract
The paper is devoted to the general methodological aspects of development of radiative heat flux sensors for various application for spacecraft. Based on the results of the executed analysis, two different algorithms for processing experimental data are proposed, relying on the methodology of inverse heat transfer problems. General patterns of mathematical models are analyzed as well. Parameters of methods for solving inverse problems are determined. The effectiveness of the algorithms developed is analyzed by means of mathematical modeling of the influence of various factors on the solution accuracy.
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Nenarokomov, A.V., Reviznikov, D.L., Neverova, D.A. et al. Absorbed Radiation Heat Flux Sensors for Orbital Spacecraft. Algorithms for Measurement Data Processing. J. Engin. Thermophys. 30, 383–403 (2021). https://doi.org/10.1134/S181023282103005X
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DOI: https://doi.org/10.1134/S181023282103005X