Numerical modeling of the flow of combustion products of the propellant containing an aluminum hydride admixture in the nozzle of a solid-propellant rocket engine has been carried out. The advantage of aluminum hydride over aluminum when used in composite solid propellants has been shown.
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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 94, No. 4, pp. 996–1000, July–August, 2021.
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Vorozhtsov, A.B., D’yachenko, N.N. Digital Twin of a High-Energy System Using Aluminum Hydride as a Fuel. J Eng Phys Thermophy 94, 972–976 (2021). https://doi.org/10.1007/s10891-021-02374-x
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DOI: https://doi.org/10.1007/s10891-021-02374-x