Ракетный двигатель  твердого топлива многократного включения  с двумя подсистемами регулирования

Aleksandr Petrovich Smorodinov; Vladimir Aleksandrovich Celischev

Repeatedly activated solid-propellant rocket engine with two regulation subsystems

Authors

Aleksandr Petrovich Smorodinov
Vladimir Aleksandrovich Celischev

Keywords:

the rocket engine of firm fuel of repeated inclusion; mathematical model; two-coherent system of automatic control; a liquid coolant.

Abstract

The approach to regulation of the Repeatedly activated solid-propellant rocket engine is presented and described. The main attention is given to maintenance of reliable shutdown of the engine and the description of intrachamber processes. Results of mathematical modelling are analysed.