Abstract: The invention concerns a low voltage-to-high voltage converter of the flyback type. The converter includes a transformer whose primary winding is linked to a supply voltage source via a switch and whose secondary winding is linked to the terminals of a capacitor via a rectifier diode. This converter includes, in a conventional manner, a secondary regulation loop which compares the output voltage appearing at the terminals of the capacitor, via a divider bridge, with a reference voltage in order to regulate the OFF time of the switch. Provision is made to maintain constant the primary energy accumulated in the transformer and the total charge time of the capacitor, regardless of the value of the supply voltage. Digital regulation of an open loop system is employed to control the ON time of the switch on the basis of the value of the supply voltage and the temperature of the converter. The invention finds particular utility in high-energy projectile firing systems.

Abstract: This detonator includes a cylindrical anvil of dielectric material bearing on one face an area of electrical contact and on the other a fusible bridge of which one end is connected to the area of electrical contact via a plugged conducting hole and of which the other end is connected to an annular conducting area around the edge of the anvil. A cylindrical hollow plug is connected to the anvil by a flanged ring soldered to the plug and to the annular conducting area of the anvil. Around this plug is fitted a cylindrical flexible contact part. A closing cylinder is soldered to the plug. Inside the plug are fitted a disk of plastic material, a barrel, and an explosive charge in a case. The assembly is closed by a cap laser welded to the closing cylinder. The invention is applicable to hermetic detonator structures for initiation in particular of warheads, propellors of rockets, missiles or other guided projectiles, or of gas generators.

Abstract: This system includes, in a projectile P bearing explosive warheads 2, 4, with their firing device 3, 5, impact detectors 1, an inertial unit 6 and a computer 7. The computer 7 determines, on the basis of the signals from the detectors 1, the instant of impact To and the angle of incidence I of the projectile on the target and, on the basis of the signals from the inertial unit 6, the speed V of the projectile at the instant of impact. Using the data V, I and the data on the type of target C, the computer 7 determines, in real time, the optimum delay with respect to the instant To for the firing of each warhead, and applies this delay to the firing command.