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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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). https://doi.org/10.1134/S0021894419040060
- measuring section
- hypersonic particle
- space debris
- contactless mode
- high-velocity collision