Contactless Measuring Section in Hypersonic Aerodynamics
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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.
Keywordsmeasuring section hypersonic particle space debris contactless mode high-velocity collision
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