Abstract A sequential algorithm for determining the temperature dependence of the bulk specific heat, the thermal conductivity, and the radiant and reflective properties of isotropic coatings on a spacecraft in… Click to show full abstract
Abstract A sequential algorithm for determining the temperature dependence of the bulk specific heat, the thermal conductivity, and the radiant and reflective properties of isotropic coatings on a spacecraft in Earth orbit is proposed. A three-dimensional formulation is selected, and Cartesian coordinates are employed. The Tikhonov regularization method is adopted.
               
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