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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: MATEC Web of conferences. 2017. Vol. 110. P. 01075 (1-4)
Type: статьи в журналах
Date: 2017
Description:
The possibility of creating high-energy materials with increased ecological purity of combustion products based on a mixed oxidizer (ammonium nitrate, ammonium perchlorate), and inorganic fuel (boron,
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Source: MATEC Web of conferences. 2017. Vol. 110. P. 01003 (1-6)
Type: статьи в журналах
Date: 2017
Description:
New scheme of the rocket motor of rocket-assisted projectile providing the increase in distance of flight due to controlled and optimal delay time of ignition of the solid-propellant charge of the SRM
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