Device for flash suppression of a rocket motor

摘要

A device in which a solid suppressant is ablated and dispensed into the gases of a main burning rocket motor in which a fast burning smokeless type solid propellant is burning to allow the suppressant to control afterburning of the gases from the burning solid propellant and the suppressant being dispensed by a sustained action igniter pyrotechnic that is also used to ignite the main motor solid propellant.