The physical mechanism of detonation combustion of nanostructured silicon with a solid-phase oxidant at a velocity of the combustion front of 1000–3000 m/s has been proposed. Thermodynamic characteristics of combustion of model solid-phase mixtures “silicon–ammonium perchlorate” with different equivalent ratios of their components have been calculated at different pressures. It has been established that a characteristic feature of detonation combustion of nanostructured silicon with a solid-phase oxidant is the stationary velocity of motion of the detonation front with a significant defect (10–15%) with respect to the Chapman–Jouguet detonation velocity. The detonation (supersonic) and subsonic regimes of combustion of nanostructured silicon with a solid-phase oxidant have been determined.
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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 93, No. 6, pp. 1492–1501, November–December, 2020.
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Krivosheyev, P.N., Mironov, V.N., Penyazkov, O.G. et al. On the Mechanism of Detonation Combustion of Nanostructured Silicon with a Solid-Phase Oxidant. J Eng Phys Thermophy 93, 1439–1448 (2020). https://doi.org/10.1007/s10891-020-02249-7
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DOI: https://doi.org/10.1007/s10891-020-02249-7