Model rockets motor for thrust production from combustion of solid propellant and hybrid fuel mixture, where system for oxidizer storage/- supply and commercial solid propellant are arranged to each other in rocket motor

摘要

A model rockets motor for thrust production from the combustion of solid propellant and hybrid fuel mixture, in which a system for an oxidizer storage/- supply and a commercial solid propellant are arranged to each other. The rocket motor after the combustion of the solid propellant, produces further thrust by independently running-off hybrid combustion of the solid propellant structure by means of inflowing of the oxidizer. Independent claims are also included for the following: (1) a release mechanism for inflowing of the oxidizer; (2) a rocket combustion chamber for combustion of a hybrid fuel mixture; and (3) equipment for thrust production.