Abstract: A payload conducted electrical weapon (“CEW”) may include a housing configured to house at least a plurality of electrodes and a signal generator. The payload CEW may be removably inserted into a bay of a launcher. The launcher may be mounted on a vehicle. The plurality of electrodes may be configured to be launched from the housing. The housing may be configured to be launched from the bay of the launcher simultaneously with or after the plurality of electrodes are launched. The signal generator may be configured to transmit a stimulus signal through the plurality of electrodes. The signal generator may be configured to transmit the stimulus signal before, during, and/or after the housing is launched.

Abstract: A drone pod may receive, stow, and launch a drone. The drone pod may include a housing, a canopy movably coupled to the housing, a platform movably coupled to the housing, and a drone bay. The drone pod may be configured to move the canopy to expose the drone bay and raise the platform relative to a floor of the drone bay to receive the drone, lower the platform toward the floor of the drone bay and move the canopy to enclose the drone bay to stow the drone, move the canopy to expose the drone bay and raise the platform relative to the floor of the drone bay to launch the drone. The drone pod may be mounted on a vehicle. A system may include a drone pod and a drone, wherein the drone pod is configured to receive, stow, and launch the drone.

Abstract: Cable retainer apparatuses for retaining a cable, and aircraft and methods including such apparatuses are provided. In one example, a cable retainer for retaining a cable proximate a surface of an aircraft includes a cable retainer. The cable retainer is configured to retain the cable. A fairing is disposed about the cable retainer and is configured to couple to the aircraft to support the cable retainer adjacent to the surface of the aircraft.

Abstract: A pressure delay mechanism is disclosed. In various embodiments, the mechanism includes a triggering mechanism operably coupled to an input signal port and to an output signal port and configured to transmit a signal from the input signal port to the output signal port and a differential pressure mechanism operably coupled to an exterior pressure input and to an interior pressure input and configured to lock the triggering mechanism during a first state of pressure difference and to unlock the triggering mechanism during a second state of pressure difference.

Abstract: Cable retainer apparatuses for retaining a cable, and aircraft and methods including such apparatuses are provided. In one example, a cable retainer for retaining a cable proximate a surface of an aircraft includes a cable retainer. The cable retainer is configured to retain the cable. A fairing is disposed about the cable retainer and is configured to couple to the aircraft to support the cable retainer adjacent to the surface of the aircraft.

Abstract: A pressure delay mechanism is disclosed. In various embodiments, the mechanism includes a triggering mechanism operably coupled to an input signal port and to an output signal port and configured to transmit a signal from the input signal port to the output signal port and a differential pressure mechanism operably coupled to an exterior pressure input and to an interior pressure input and configured to lock the triggering mechanism during a first state of pressure difference and to unlock the triggering mechanism during a second state of pressure difference.

Abstract: The present disclosure provides a low energy explosive transfer adapter. The low energy explosive transfer adapter may comprise an adapter housing comprising a firing pin chamber situated within the adapter housing comprising an inlet and a stopping surface opposite the inlet. The low energy explosive transfer adapter may further comprise a primer chamber connected to the firing pin chamber and an output tube connected to the primer chamber.