METHOD FOR SUPPLYING A MISSILE ENGINE WITH A STORABLE PROPELLANT

摘要

The present invention relates to a method for supplying a missile engine with a storable propellant, which includes the consecutive steps of: 1) generating combustion gas by combustion of a pyrotechnic charge, and pressurising said storable propellant by means of said combustion gas; and then 2) selectively supplying said pressurised storable propellant to said engine. In a characteristic manner, said method is implemented with a pyrotechnic charge which generates combustion gases essentially made up of hydrogen.