Modeling the Effect of a Temperature Shock on the Rotational Motion of a Small Spacecraft, Considering the Possible Loss of Large Elastic Elements Stability

The paper investigates the issues of a small spacecraft large elastic elements temperature shock influence within framework two-dimensional model thermal conductivity, taking into account possible loss stability during shock. causes additional movements sections. work explores this movement. results were obtained using Sophie Germain equation for thin plates. thermoelasticity problem is solved, in which parameters relative motion elements, including stability, are estimated. finite element method was used to solve problem. Additional microaccelerations resulting from Recommendations given avoid can be design technological spacecraft. In particular, when selecting elements. selection these parameters, work, will help