DESIGNING A HEAT SHIELD FROM CARBON AEROGEL-BASED COMPOSITE MATERIAL FOR SPACE VEHICLES

An algorithm of optimum designing a multilayer thermal insulation, based on a carbon aerogel reinforced with a highly porous cellular carbon material, with account of the dependence of the thermophysical properties of the composite material on the microstructure of the reinforcing fi ller is presented. The practical application of the indicated algorithm is illustrated by the example of solving the problem on designing a three-layer heat shield for a solar probe

Author:  O. M. Alifanov, S. A. Budnik, A. V. Nenarokomov, M. O. Salosina
Keywords:  optimization, multilayer heat shield, carbon aerogel, highly porous cellular material
Page:  1788