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Contactless Measuring Section in Hypersonic Aerodynamics


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.

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Correspondence to S. I. Gerasimov.

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Original Russian Text © S.I. Gerasimov, V.I. Erofeev, A.G. Sirotkina, A.V. Zubankov, R.V. Gerasimova.

Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 60, No. 4, pp. 56–60, July–August, 2019.

This work was supported by the Russian Foundation for Basic Research (Grant Nos. 17-08-01096 and 18-29-10073).

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Gerasimov, S.I., Erofeev, V.I., Sirotkina, A.G. et al. Contactless Measuring Section in Hypersonic Aerodynamics. J Appl Mech Tech Phy 60, 639–643 (2019).

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  • measuring section
  • hypersonic particle
  • space debris
  • contactless mode
  • high-velocity collision