Non-Contact Measuring Section in the Problem of Hypersonic Aerodynamics
S. I. Gerasimov1,2,3,4, V. I. Erofeev4, A. G. Sirotkina2, A. V. Zubankov2, R. V. Gerasimova1,2
1All-Russian Research Institute of Experimental Physics, Sarov, 607190, Russia
2Sarov Institute of Physics and Technology, Sarov, 607186, Russia
3Alekseev Nizhny Novgorod State Technical University, Nizhny Novgorod, 603950, Russia
4Institute for Problems of Mechanical Engineering of the Russian Academy of Sciences, Nizhny Novgorod, 603024, Russia
Keywords: измерительное сечение, гиперзвуковая частица, космический 'мусор', бесконтактный способ, высокоскоростное соударение, measuring section, hypersonic particle, space debris, noncontact mode, high-velocity collision
Abstract
This paper considers the possibility of using measuring sections with inductive sensors to detect hypersonic particles in time in the simulation of collisions of objects with space debris. A method for determining the average velocity of hypersonic particles simulating the 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 the spacecraft.
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