System for testing burning process of the rocket solid fuel charge containing powdered metal, placed in the combustion chamber with the ignition circuit and pressure sensor, with its own source of magnetic field

摘要

the subject invention is a testing process combustion load standing rocket fuel (1) containing the powdered metal placed in the combustion chamber (2) of the ignition system (3) and a pressure sensor (5), having a magnetic field source (6) located outside the chamber. combustion (2).this system is used to study effect of magnetic field on the combustion process, especially on the burning rate of rocket fuel (1). system allows to examine the impact of magnetic field on the combustion process of solid rocket fuels (1) containing powdered metal, especially on their speed of combustion.