부산대학교 도서관

This paper considers the possibility of using measuring sections with inductive sensors to detect hypersonic particles in time in modeling collisions of objects with space debris. A method for determining the average velocity of hypersonic particles simulating space debris and a method of starting the recording equipment for optical contactless detection of these particles are proposed. Results of experimental studies of the interaction of particles with a simulator of the mesh shield of spacecraft. [ABSTRACT FROM AUTHOR]