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Source: Combustion, explosion, and shock waves. 2017. Vol. 53, № 6. P. 634-640
Type: статьи в журналах
Date: 2017
Description:
A method for performance optimization of a standard-flow hybrid rocket engine is considered. The method is based on inserting an additional amount of an oxidizer into a solid propellant with a prescri
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Source: 12th International Conference "Gas Discharge Plasmas and Their Applications" GDP 2015, September 6-11, 2015, Tomsk, Russia : Abstracts. Tomsk, 2015. P. 147
Type: статьи в сборниках
Date: 2015