Abstract:
AN IGNITION SYSTEM POSITIONED BETWEEN THE COMBUSTION CHAMBER OF A GAS GENERATOR HAVING A SOLID PROPELLANT GRAIN THEREIN AND THE COMBUSTION CHAMBER OF A SOLID PROPELLANT ROCKET MOTOR HAVING SELECTIVE ZONING CAPABILITIES SO THAT WHEN THE IGNITION SYSTEM IS OPERATED THE COMBUSTION GASES FROM THE COMBUSTION CHAMBER OF THE SOLID PROPELLANT ROCKET MOTOR WILL ENTER THE COMBUSTION CHAMBER IN THE GAS GENERATOR AND IGNITE THE SOLID PROPELLANT GRAIN THEREIN.
Abstract:
A RUPTURABLE MEMBRANE SEAL ASSEMBLY FOR USE IN SEPARATING THE ZONES OFA SOLID PROPELLANT GRAIN IN A SOLID PROPELLANT ROCKET MOTOR HAVING SELECTIVE ZONING CAPABILITIES THAT WILL BE DISINTEGRATED, WHEN THE PRESSURE IN A GAS GENERATOR SEPARATED FROM THE SOLID PROPELLANT ROCKET MOTOR BY THE MEMBRANE SEAL ASSEMBLY BECOMES GREATER THAN THE PRESSURE IN THE SOLID PROPELLANT ROCKET MOTOR.