A Munitions Payload Delivery System (MPDS) is provided. One embodiment of the MPDS comprises a multi-rotor drone configured to carry a munition in the form of a HEDP linear-shaped charge or Armor Piercing munition or other-shaped munition. The drone, in one embodiment, includes a camera that provides a remote operator with a real-time video feed so the operator can pilot the drone to a specific target on a battlefield. Once a target is selected, the operator ignites the munition by flying the drone into the target, landing the drone on the target, or activating a radio fire button. In one embodiment, each of these mechanisms closes a switch on board the drone connecting a voltage to a blasting cap inside the payload.

A Munitions Payload Delivery System (MPDS) is provided. One embodiment of the MPDS comprises a multi-rotor drone configured to carry a munition in the form of a HEDP linear-shaped charge or Armor Piercing munition or other-shaped munition. The drone, in one embodiment, includes a camera that provides a remote operator with a real-time video feed so the operator can pilot the drone to a specific target on a battlefield. Once a target is selected, the operator ignites the munition by flying the drone into the target, landing the drone on the target, or activating a radio fire button. In one embodiment, each of these mechanisms closes a switch on board the drone connecting a voltage to a blasting cap inside the payload.

Various types of structures, along with associated systems, are disclosed herein and configured for responding to an energy wave for changing a state of a mechanism to which said structures are operatively coupled. In at least one embodiment, the structure provides a material selectively changeable upon exposure to the energy wave to cause at least a portion of the material to mechanically degrade from a first state to a second state. When the material is in the first state, the material forms a mechanical or electrical link with the mechanism such that a force or an electrical current can be transmitted through the structure. When the material is in the second state, degradation of at least the portion of the material disrupts the mechanical or electrical link and inhibits transmission of the force or electrical current through the structure.

Various types of structures, along with associated systems, are disclosed herein and configured for responding to an energy wave for changing a state of a mechanism to which said structures are operatively coupled. In at least one embodiment, the structure provides a material selectively changeable upon exposure to the energy wave to cause at least a portion of the material to mechanically degrade from a first state to a second state. When the material is in the first state, the material forms a mechanical or electrical link with the mechanism such that a force or an electrical current can be transmitted through the structure. When the material is in the second state, degradation of at least the portion of the material disrupts the mechanical or electrical link and inhibits transmission of the force or electrical current through the structure.

A system and method are provided for safe arming a flying machine that carries an explosive device. Once armed, the flying machine can provide air defense against a target (e.g., an unwanted aircraft) by using the explosive device to kinetically intercept the unwanted aircraft. The flying machine can include an explosive device, an arming device, and one or more sensors (e.g., a 9-axis inertial measurement unit). By processing the sensor data, the flying machine determines whether arming criteria have been satisfied (e.g., the flying machine has attained a desired altitude or undergone a specified pattern of accelerations), and when the arming criteria are satisfied the flying machine arms the explosive device by completing a detonation path. If the explosive device is not detonated, the system returns to a safe state before the flying machine back to its origin.

A system and method are provided for safe arming a flying machine that carries an explosive device. Once armed, the flying machine can provide air defense against a target (e.g., an unwanted aircraft) by using the explosive device to kinetically intercept the unwanted aircraft. The flying machine can include an explosive device, an arming device, and one or more sensors (e.g., a 9-axis inertial measurement unit). By processing the sensor data, the flying machine determines whether arming criteria have been satisfied (e.g., the flying machine has attained a desired altitude or undergone a specified pattern of accelerations), and when the arming criteria are satisfied the flying machine arms the explosive device by completing a detonation path. If the explosive device is not detonated, the system returns to a safe state before the flying machine back to its origin.

A fuse-less ignition system for fireworks. An ignitor module is provided that is insertable into a firework and includes: a first end having an interface adapted to reside on an exterior surface of the firework for receiving a plug; a set of electrical contacts adapted to receive electricity from the plug; a heat element coupled to the electrical contacts and adapted to heat in response to received electricity; and a cavity adjacent to the heat element containing a pyrotechnic material, the pyrotechnic material adapted to ignite in response to a heating of the heat element.

A fuse-less ignition system for fireworks. An ignitor module is provided that is insertable into a firework and includes: a first end having an interface adapted to reside on an exterior surface of the firework for receiving a plug; a set of electrical contacts adapted to receive electricity from the plug; a heat element coupled to the electrical contacts and adapted to heat in response to received electricity; and a cavity adjacent to the heat element containing a pyrotechnic material, the pyrotechnic material adapted to ignite in response to a heating of the heat element.

A method of communicating in a blast system which includes the steps of transmitting timing signals from a master transceiver to a plurality of local transceivers, in response, at each local transceiver, defining a succession of micro-slots and calculating a size of a respective bin which is associated with each micro-slot, transmitting a packet from the master transceiver, at each local transceiver calculating a uniform random value, identifying the bin in which the uniform random value is located and during the micro-slot which is associated with the identified bin, if no transmission of a reply signal from any other local transceiver is detected, in response to the packet transmitting a reply signal from the local transceiver to the master transceiver.

A method of communicating in a blast system which includes the steps of transmitting timing signals from a master transceiver to a plurality of local transceivers, in response, at each local transceiver, defining a succession of micro-slots and calculating a size of a respective bin which is associated with each micro-slot, transmitting a packet from the master transceiver, at each local transceiver calculating a uniform random value, identifying the bin in which the uniform random value is located and during the micro-slot which is associated with the identified bin, if no transmission of a reply signal from any other local transceiver is detected, in response to the packet transmitting a reply signal from the local transceiver to the master transceiver.