Digital Twin of a High-Energy System Using Aluminum Hydride as a Fuel View Full Text


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Article Info

DATE

2021-07

AUTHORS

A. B. Vorozhtsov, N. N. D’yachenko

ABSTRACT

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.

PAGES

972-976

Identifiers

URI

http://scigraph.springernature.com/pub.10.1007/s10891-021-02374-x

DOI

http://dx.doi.org/10.1007/s10891-021-02374-x

DIMENSIONS

https://app.dimensions.ai/details/publication/pub.1140707219


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