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.

作者简介

S. Gerasimov

All-Russian Research Institute of Experimental Physics (VNIIEF); Sarov Institute of Physics and Technology—Branch of the National Research Nuclear University (MEPhI); Alekseev Nizhny Novgorod State Technical University; Institute for Problems of Mechanical Engineering—Branch of the Institute of Applied Physics

编辑信件的主要联系方式.
Email: s.i.gerasimov@mail.ru
俄罗斯联邦, Sarov, 607190; Sarov, 607186; Nizhny Novgorod, 603950; Nizhny Novgorod, 603024

V. Erofeev

Institute for Problems of Mechanical Engineering—Branch of the Institute of Applied Physics

Email: s.i.gerasimov@mail.ru
俄罗斯联邦, Nizhny Novgorod, 603024

A. Sirotkina

Sarov Institute of Physics and Technology—Branch of the National Research Nuclear University (MEPhI)

Email: s.i.gerasimov@mail.ru
俄罗斯联邦, Sarov, 607186

A. Zubankov

All-Russian Research Institute of Experimental Physics (VNIIEF); Sarov Institute of Physics and Technology—Branch of the National Research Nuclear University (MEPhI)

Email: s.i.gerasimov@mail.ru
俄罗斯联邦, Sarov, 607190; Sarov, 607186

R. Gerasimova

Sarov Institute of Physics and Technology—Branch of the National Research Nuclear University (MEPhI)

Email: s.i.gerasimov@mail.ru
俄罗斯联邦, Sarov, 607186

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