In the present study the results of mathematical modeling of impingement plumes with landing site of "ExoMars" landing platform are shown. The gas-dynamic parameters while landing platform impingement plumes with surface of Mars were obtained at an altitude of 1; 0,5; 0,3 meter. The thrust at this altitude of four thrusters was set to 7648 N and 54936 N. These results allow further evaluation of thermal and power loads occur on the surfaces of the landing platform and the Martian surface as the result of the impingement of a thruster plume on surface.
Перспективы развития фундаментальных наук : сборник научных трудов XIV Международной конференции студентов, аспирантов и молодых ученых, Россия, Томск, 25-28 апреля 2017 г.. Томск, 2017. Т. 1 : Физика. С. 144-146