Correction: [Data-Driven Modelling of Aerothermo dynamic Loads during Atmospheric Re-entry] (AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023)

Correction Notice In addition to the provided Validation in Section V of the paper given for the continuum flow regime test case, an addendum is provided here with validation results for the rarefied test cases to complete this study. Leave One Out Analysis The results for the Leave One Out analysis for the rarefied regime CubeSat test case are shown in Fig. 1. Like with the ATV test case, the results are visualized on the attitude unit sphere and the error maps shown here correspond to the case with maximum absolute error for the respective integral quantity. (Figure Presented).