Designing a Heat Shield from Carbon Aerogel-Based Composite Material for Space Vehicles
摘要
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 filler 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.