TY  - SER
AU  - Arkhipov,Vladimir A.
AU  - Zolotorev,Nikolay N.
AU  - Perfilieva,Ksenia G.
TI  - Performance optimization of a standard-flow hybrid rocket engine
KW  - гибридные ракетные двигатели
KW  - твердые ракетные топлива
KW  - статьи в журналах
N1  - Библиогр.: 20 назв
N2  - 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 prescribed distribution of the oxidizer mass fraction along the solid propellant charge. An analytical dependence is derived for the oxidizer fraction distribution that ensures uniform combustion and high efficiency of the solid propellant charge
UR  - http://vital.lib.tsu.ru/vital/access/manager/Repository/vtls:000621911
ER  -