When analyzing the thermal stress and deformation of satellites in orbit, traditional numerical methods, such as finite difference element, are expensive time-consuming. To improve computational efficiency, we propose a deep-learning based surrogate to immediately predict satellite with given temperature field, where U-Net is employed learn end-to-end mapping from field deformation. A data set ...

Thermomechanical analysis of the space shuttle tile thermal protection system (TPS) subjected to damage is conducted using the finite element method. The thermal and structural response of the damaged configurations are compared with the undamaged configuration to determine the relative effects of damage on the thermal protection capability and the induced thermal stresses in the TPS. The TPS i...

Thermomechanical analysis of the space shuttle tile thermal protection system (TPS) subjected to damage is conducted using the finite element method. The thermal and structural response of the damaged configurations are compared with the undamaged configuration to determine the relative effects of damage on the thermal protection capability and the induced thermal stresses in the TPS. The TPS i...