Modeling the deformation of an elastic element of a small spacecraft in its plane during temperature shock

A basic mathematical model of the deformation a large elastic element small spacecraft in its plane is constructed. Deformations are caused by temperature shock after leaves Earth’s shadow on solar portion orbit. The used to conduct computational experiment with aim assessing perturbations acting due shock. distribution during thermal described one-dimensional conductivity. classical theory thin plates determine deformations. results estimation disturbing factors obtained as result for spacecraft. These indicate need compensate impact technological data can be design space-craft purposes.