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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: Известия высших учебных заведений. Физика. 2014. Т. 57, № 12. С. 155-157
Type: статьи в журналах
Date: 2014