2.Introduction: During the second half of 20 th century, non-isothermal problems of the theory of elasticity became increasingly important. This is due to their wide application in diverse fields. The high velocities of modern aircraft give rise to aerodynamic heating, which produces intense thermal stresses that reduce the strength of aircraft structure. Recently D. T. Solanke, M. H. Durge have studied the thermal stresses in thin cylinder with Dirichlet's, Neumann's, Robin's boundary condition and in thin hollow cylinder with Dirichlet's, Neumann's boundary condition. Now authors in this present paper determine temperature, thermal stresses, in thin hollow cylinder with Robis's boundary condition, determined by