F42C15/42

Wireless detonator assembly

A wireless detonator assembly which includes a detonator, a receiver, a printed circuit board with a stored key which is hardwired onto the board during manufacture of the detonator assembly and control logic which allows the detonator to be fired only if the control logic extracts from a signal, received by the receiver, a reference key which is identical to the stored key.

Wireless detonator assembly

A wireless detonator assembly which includes a detonator, a receiver, a printed circuit board with a stored key which is hardwired onto the board during manufacture of the detonator assembly and control logic which allows the detonator to be fired only if the control logic extracts from a signal, received by the receiver, a reference key which is identical to the stored key.

Area denial communication latency compensation

An area denial system may be operationally placed with communication latency compensation. The area denial system may include a plurality of munitions, one or more sensor devices, and a command and control unit, networked together and having a command and control latency for communication between the command and control unit and the remainder of the area denial system. Latency compensation may include determining a first target position, determining a first predicted position area for the target using the command and control latency and the first target position, receiving an authorization to arm one or more of the munitions, determining a second target position, and determining that the second target position is outside a threshold distance from a first authorized munition of the one or more authorized munitions, and in response, de-authorizing the first authorized munition.

Area denial communication latency compensation

An area denial system may be operationally placed with communication latency compensation. The area denial system may include a plurality of munitions, one or more sensor devices, and a command and control unit, networked together and having a command and control latency for communication between the command and control unit and the remainder of the area denial system. Latency compensation may include determining a first target position, determining a first predicted position area for the target using the command and control latency and the first target position, receiving an authorization to arm one or more of the munitions, determining a second target position, and determining that the second target position is outside a threshold distance from a first authorized munition of the one or more authorized munitions, and in response, de-authorizing the first authorized munition.

Electronic ignition circuit

The present disclosure describes an electronic ignition circuit (EIC) for controlling at least one detonator. The EIC may include a protection circuit, an input circuit coupled to the protection circuit, a logic circuit electrically coupled to the input circuit, and an ignition circuit electrically coupled to the logic circuit. The protection circuit may include at least one of a fuse, a circuit breaker and an automatic switch. The logic circuit may include an answer back circuit, and a switching circuit adapted to switch to the next detonator or igniter. The ignition circuit may include a capacitor charging circuit, a capacitor discharge circuit to discharge a firing capacitor through a fuse head, and a shot detection circuit adapted to measure a voltage across the firing capacitor before discharging through the fuse head and to measure a voltage after discharging through the fuse head.

Electronic ignition circuit

The present disclosure describes an electronic ignition circuit (EIC) for controlling at least one detonator. The EIC may include a protection circuit, an input circuit coupled to the protection circuit, a logic circuit electrically coupled to the input circuit, and an ignition circuit electrically coupled to the logic circuit. The protection circuit may include at least one of a fuse, a circuit breaker and an automatic switch. The logic circuit may include an answer back circuit, and a switching circuit adapted to switch to the next detonator or igniter. The ignition circuit may include a capacitor charging circuit, a capacitor discharge circuit to discharge a firing capacitor through a fuse head, and a shot detection circuit adapted to measure a voltage across the firing capacitor before discharging through the fuse head and to measure a voltage after discharging through the fuse head.

System and Method for Autonomous or Remote Controlled Destruction of Stored Information or Components
20200097668 · 2020-03-26 · ·

A system and method are provided for the destruction of electronically stored information and/or components that incorporated sensitive technology or that contain sensitive information upon the occurrence of one or more predetermined events. The system and method of the present invention is particularly suited for the safeguarding of electronically stored information and/or classified technology in systems deployed in an operational environment. The system and method of the present invention be incorporated into drones, full size aircraft, any type of vehicle, mines, missiles, torpedos, bombs, phones, cameras, robots, satellites or other spacecraft, computers, hard drives, thumb drives, switches, routers, bugs, brief cases, safes, and generally any device that utilizes components on which sensitive data is stored or components that utilize technology that should only be accessed by authorized personnel.

System and Method for Autonomous or Remote Controlled Destruction of Stored Information or Components
20200097668 · 2020-03-26 · ·

A system and method are provided for the destruction of electronically stored information and/or components that incorporated sensitive technology or that contain sensitive information upon the occurrence of one or more predetermined events. The system and method of the present invention is particularly suited for the safeguarding of electronically stored information and/or classified technology in systems deployed in an operational environment. The system and method of the present invention be incorporated into drones, full size aircraft, any type of vehicle, mines, missiles, torpedos, bombs, phones, cameras, robots, satellites or other spacecraft, computers, hard drives, thumb drives, switches, routers, bugs, brief cases, safes, and generally any device that utilizes components on which sensitive data is stored or components that utilize technology that should only be accessed by authorized personnel.

Multipoint payload release system

Networked initiation systems for hold-down and release mechanisms (HDRMs) are described. The systems include a control unit, a plurality of firing control units operably connected to and in communication with the control unit, wherein each firing control unit has at least one HDRM operably connected thereto, and wherein each firing control unit is individually addressable by the control unit over an interface bus to enable selective operation of the HDRMs operably connected to the firing control units.

Multipoint payload release system

Networked initiation systems for hold-down and release mechanisms (HDRMs) are described. The systems include a control unit, a plurality of firing control units operably connected to and in communication with the control unit, wherein each firing control unit has at least one HDRM operably connected thereto, and wherein each firing control unit is individually addressable by the control unit over an interface bus to enable selective operation of the HDRMs operably connected to the firing control units.