An ordnance delivery system has a cable deployable by a winch from an aircraft, an end effector comprising controllable thrusters attached at a deployed end of the cable, first control circuitry in the end effector and second control circuitry in the aircraft, the first and second control circuitry in communication, an ordinance delivery region in the end effector carrying ordnance for delivery on a target, and a release mechanism by which the ordnance is released to fall on the target. The aircraft is piloted to a position over a target, the end effector is controlled to position more accurately over the target; and the release mechanism is activated, releasing the ordnance to fall on the target.

A jammer which eliminates the need for a bobtail in a forward deployment. The jammer has an outwardly extending boom with a table at the distal end of the boom. The table can mount upwardly extending cradles suitable for temporarily holding cargo, such as a munition, during transport and positioning on the underside of an aircraft wing. The table also holds an upstanding pintle hook. The pintle hook provides for attachment of the jammer to a trailer for towing. Using the jammer for both towing of a trailer and positioning of cargo using the boom eliminates the need for a bobtail, conserving both cargo space and payload weight during deployment.

A jammer which eliminates the need for a bobtail in a forward deployment. The jammer has an outwardly extending boom with a table at the distal end of the boom. The table can mount upwardly extending cradles suitable for temporarily holding cargo, such as a munition, during transport and positioning on the underside of an aircraft wing. The table also holds an upstanding pintle hook. The pintle hook provides for attachment of the jammer to a trailer for towing. Using the jammer for both towing of a trailer and positioning of cargo using the boom eliminates the need for a bobtail, conserving both cargo space and payload weight during deployment.

A system for refueling has a boom having a rigid portion and, extendible portion and a fuel nozzle at an end of the extendible portion, the fuel nozzle mates with a port on an aircraft. Control circuitry in the tanker aircraft has input elements by which an operator controls actuators moving the boom left, right and up and down, and a first imaging device proximate the end of the extendible portion of the boom, capturing images and transmitting the captured images to the control circuitry, where the images are displayed on a monitor visible to the operator. The operator controls extension and attitude of the fuel nozzle at the end of the extendible portion, according to the images displayed, mating the fuel nozzle with the refueling port, and transferring fuel from the tanker aircraft to the aircraft to be refueled.

A system for refueling has a boom having a rigid portion and, extendible portion and a fuel nozzle at an end of the extendible portion, the fuel nozzle mates with a port on an aircraft. Control circuitry in the tanker aircraft has input elements by which an operator controls actuators moving the boom left, right and up and down, and a first imaging device proximate the end of the extendible portion of the boom, capturing images and transmitting the captured images to the control circuitry, where the images are displayed on a monitor visible to the operator. The operator controls extension and attitude of the fuel nozzle at the end of the extendible portion, according to the images displayed, mating the fuel nozzle with the refueling port, and transferring fuel from the tanker aircraft to the aircraft to be refueled.

There is provided an arming apparatus for a store, the apparatus comprising: a first attachment system and a second attachment system; a linking connector coupled with the first attachment system and the second attachment system; and an arming connector coupled with the linking connector and a first fuze input of the store; wherein each of the first attachment system and the second attachment system comprises: an arming unit; a first frangible connector coupled with the arming unit and the linking connector; and a second frangible connector coupled with the linking connector and the store.

A 1-to-N munitions adapter that includes a physical launcher interface, a physical munitions interface, and electronic control circuitry. The physical launcher interface is operable to connect the 1-to-N munitions adapter to a single munition launcher that is i) configured and arranged to carry and launch a single munition of a first type, and ii) integrated to an airborne platform. The physical munitions interface is operable to connect the 1-to-N munitions adapter to multiple munitions of a second type. The 1-N munitions adapter i) emulates a control interface of a single munition of the first type to the single munition launcher, in part by identifying the 1-to-N munitions adapter to the single munition launcher as a single munition of the first type, and ii) selectively controls the release of munitions of the second type while the airborne platform is in flight in response to signals received from the single munition launcher.

A 1-to-N munitions adapter that includes a physical launcher interface, a physical munitions interface, and electronic control circuitry. The physical launcher interface is operable to connect the 1-to-N munitions adapter to a single munition launcher that is i) configured and arranged to carry and launch a single munition of a first type, and ii) integrated to an airborne platform. The physical munitions interface is operable to connect the 1-to-N munitions adapter to multiple munitions of a second type. The 1-N munitions adapter i) emulates a control interface of a single munition of the first type to the single munition launcher, in part by identifying the 1-to-N munitions adapter to the single munition launcher as a single munition of the first type, and ii) selectively controls the release of munitions of the second type while the airborne platform is in flight in response to signals received from the single munition launcher.

A container retention and release apparatus includes an actuator a swaybrace and retention assembly pivotally coupled to the actuator. The swaybrace and retention assembly pivot relative to the actuator between a first position to retain a container and a second position to release the container.

A cavity system, comprising: a cavity (2) comprising a cavity opening; and an acoustically reflective structure (18, 20) located at least partially within the cavity (2), the acoustically reflective structure (18, 20) comprising one or more acoustically reflective surfaces (24, 26, 30, 32), each acoustically reflective surface (24, 26, 30, 32) being oblique to a plane of the cavity opening (27). The one or more acoustically reflective surfaces (24, 26, 30, 32) may be arranged to reflect incident acoustic waves out of the cavity opening while avoiding reflection into a region (48) at or proximate to a leading edge (14) of the cavity (2).