Raytheon Company

L3 Fuzing and Ordnance Systems

Tim B Bonbrake

Bradley M Biggs

Jesse T Waddell

Henri Y Kim

Kim L Christianson

Noah Desch

Nicole Quackenbush

Nicole M Quackenbush

A shock mitigation assembly for a penetrating explosive weapon having a first explosive charge and a second explosive charge includes an electronic circuit card having an electronic circuit formed therein, a weight attached to the circuit card to form a circuit card subassembly, a housing enclosing the subassembly, and a hyperelastic material between the housing and the subassembly for internal shock mitigation. The hyperelastic material has a modulus of elasticity that remains elastic characteristics with shock, temperature, or a combination of shock and temperature. The housing may include a casing and a cover with corresponding features that mate with one another and prevent separation of the cover from the casing. The casing also may have an external spiral flange that overlaps an internal spiral flange of a support for the casing, with a hyperelastic material between the casing and support for external shock mitigation.

Shock mitigation assembly for a penetrating weapon

There is a firing and arming system, such as an activation system, of a munition for quickly and accurately activating a warhead or a propulsion system of the activation system. An initiator interface of the activation system activates the warhead or propulsion system. At least one power source is included in the activation system to provide the initial power for activation of the initiator interface and subsequent activating of the respective warhead or propulsion system. Logic elements are communicatively disposed between the at least one power source and a flux compression generator circuit to control activation of the generator. The flux compression generator circuit is at least partially detonated to transform current received from the at least one power source into sufficient current for activating the initiator interface.

Method and apparatus for executing a weapon safety system utilizing explosive flux compression

The safing system employs a multi-axis accelerometer system and multi-axis gyroscope system and a processor that is programmed to iteratively read acceleration data from the accelerometer system and apply a multi-axis rotation on the acceleration data using gyroscope data iteratively read from the gyroscope system to generate rotationally corrected acceleration data and further programmed to calculate a cumulative distance measure using the rotationally corrected acceleration data. The processor then compares the cumulative distance measure with a predetermined reference measure and to issue a control signal to enable arming of the device when the cumulative distance measure exceeds the reference measure.

Fuze safing system

A system includes a first arm switch, a voltage multiplier device connected in series with the first arm switch, and a first intermediate voltage detector portion communicatively connected to the sequence of events logic portion, the first intermediate voltage detector portion operative to determine whether a first voltage signal is greater than a first threshold voltage value and responsive to determining that the first voltage signal is greater than the first threshold voltage value affect an actuation of the first arm switch and output a first arm signal.

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Tucson, AZ, United States of America

Tim B Bonbrake