Disclosed is a method of providing an ingition system for substantially simultaneously and uniformily igniting all the internal burning surfaces of a large propellant grain of the internal burning grain type that is employed in an upper stage advanced missile interceptor. The propellant grain to be ignited is also of the type which requires support for reinforcing the grain during high acceleration loads especially before the interceptor stage motor is pressurized. The means for igniting the large propellant grain is comprised of high-velocity deflagrati...
A method of providing an ignition system for substantially simultaneously and uniformly igniting all the internal burning surfaces of a large solid propellant grain which has been cast and cured for use as an upper stage rocket motor designed with an internal burning grain configuration for an advanced missile interceptor, said large propellant grain because of the inadequancy of its mechanical properties requiring a supporting means to prevent flow and break up of the propellant grain under acceleration loads especially before said upper stage rocket mo...
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