Investigating the temperature field of large elastic elements of a small spacecraft for the Earth remote sensing to assess the effect of a temperature shock on its rotational motion

The paper considers the effect of the temperature shock of small spacecraft large elastic elements during its immersion in the Earth's shadow. The one-dimensional problem of thermal conductivity is solved. The results of numerical simulation are presented. The results of the work can be used to solve the problem of ensuring the required orientation of the Earth remote sensing spacecraft, as well as transporting space debris to burial orbits.