Abstract: According to one embodiment of the disclosure, a remote explosive detonation system includes a transmitter and at least one receiver having a detonator. The transmitter transmits an electro-magnetic signal having a transmitter identification code that may be received by the receiver. The receiver initiates the detonator if the transmitter identification code matches an internal identification code stored in the receiver.

Abstract: According to one embodiment, a chaff pod includes at least two dispensers disposed within a chaff pod housing. Each of the dispensers has a surface defining an opening through which a number of countermeasures may be dispensed. The dispensers are configured to be coupled to the aircraft. The first dispenser directs countermeasures in a first direction, and the second dispenser directs countermeasures in a second direction. The difference between the first direction and the second direction form a relative angle.

Abstract: Methods and apparatus for a cable retractor to facilitate removal of a cable connector from an item after release from a vehicle. In one embodiment, the cable retractor pulls in the connector after the item is released.

Abstract: Methods and apparatus for a cable retractor to facilitate removal of a cable connector from an item after release from a vehicle. In one embodiment, the cable retractor pulls in the connector after the item is released.

Abstract: A carriage and ejection assembly for retaining different types of stores to an aircraft and selectively ejecting a carried one of the stores away from the aircraft is disclosed. The assembly can include a sway brace having at least one contact location for each type of store, wherein during ejection of the carried store by actuation of the sway brace, the at least one contact location corresponding to the carried store applies a pitch downward moment to the carried store. Another feature of the assembly can include a direct connection of the sway brace to a moveable part of an ejection actuator. Another feature of the assembly can include independent latching and unlatching of plural store retaining hooks of the assembly. Another feature can include a compressor for pressurizing a piston of the assembly that is carried by the aircraft. Yet another feature can include a hook release actuator placed in series with and upstream of an ejector actuator.