Disclosed is a device and method to load stores on an aircraft. The device may include a controller configured to: assign one or more stores to the aircraft; and control at least one actuator to: control a position of the aircraft; load the one or more stores onto one or more corresponding lift portions; position the one or more stores relative to a position of the aircraft determined in accordance with sensor information from at least one sensor; and secure the one or more stores to the aircraft.

Disclosed is a device and method to load stores on an aircraft. The device may include a controller configured to: assign one or more stores to the aircraft; and control at least one actuator to: control a position of the aircraft; load the one or more stores onto one or more corresponding lift portions; position the one or more stores relative to a position of the aircraft determined in accordance with sensor information from at least one sensor; and

secure the one or more stores to the aircraft.

Disclosed is a device and method to load stores on an aircraft. The device may include a controller configured to: assign one or more stores to the aircraft; and control at least one actuator to: control a position of the aircraft; load the one or more stores onto one or more corresponding lift portions; position the one or more stores relative to a position of the aircraft determined in accordance with sensor information from at least one sensor; and

secure the one or more stores to the aircraft.

A jaw pivoting about an axis for clamping the shell, a lower end of the jaw receives the shell to allow closure. The notch intended to interfere with a catch of a cam to retain the jaw in the closed position. The cam is rigidly connected to a pivoting lever which allows the catch to be moved from the path of the notch to allow the jaw to open. The lever is to be pivotally activated through the force of an external component. The device includes a first and second spring each acting on the lever in an opposing manner, the second spring being stiffer than the first spring. The effect of the first spring is to lift the lever. The second spring counters the action of the first spring in order to delay the lifting of the lever and the catch when removing the component.

Apparatus and associated methods relate to automatically loading a plurality of hazardous entities into a hazardous-entity container. Such automatic loading is performed by: i) lifting a selected hazardous entity of a plurality of hazardous entities from a stowed position to an elevation of a corresponding hazardous-entity portal of the hazardous-entity container; ii) sensing relative alignment the selected hazardous entity with respect to the corresponding hazardous-entity portal iii) aligning the selected hazardous entity with the corresponding hazardous-entity portal based on the relative alignment sensed by the alignment sensor; iv) evaluating whether an insertion condition is met based at least in part on the relative alignment sensed by the alignment sensor; and v) inserting the selected hazardous entity into its corresponding hazardous-entity portal if the insertion condition is met.

Apparatus and associated methods relate to automatically loading a plurality of hazardous entities into a hazardous-entity container. Such automatic loading is performed by: i) lifting a selected hazardous entity of a plurality of hazardous entities from a stowed position to an elevation of a corresponding hazardous-entity portal of the hazardous-entity container; ii) sensing relative alignment the selected hazardous entity with respect to the corresponding hazardous-entity portal iii) aligning the selected hazardous entity with the corresponding hazardous-entity portal based on the relative alignment sensed by the alignment sensor; iv) evaluating whether an insertion condition is met based at least in part on the relative alignment sensed by the alignment sensor; and v) inserting the selected hazardous entity into its corresponding hazardous-entity portal if the insertion condition is met.

A mounting platform is provided for securing munitions. The platform includes a flat plate, a front block and a rear block. The plate includes a plurality of cutout holes. The front block has a first saddle disposed between first flanking ends and at least one extension at one of the flanking ends for inserting into a first opening of the cutouts. The rear block has a second saddle disposed between second flanking ends at least one extension for inserting into a second opening of the cutouts. The munitions are disposable atop the first and second saddles of the front and rear blocks. The munitions are restrained axially against a rear stop block and laterally by the saddles and straps.

A mounting platform is provided for securing munitions. The platform includes a flat plate, a front block and a rear block. The plate includes a plurality of cutout holes. The front block has a first saddle disposed between first flanking ends and at least one extension at one of the flanking ends for inserting into a first opening of the cutouts. The rear block has a second saddle disposed between second flanking ends at least one extension for inserting into a second opening of the cutouts. The munitions are disposable atop the first and second saddles of the front and rear blocks. The munitions are restrained axially against a rear stop block and laterally by the saddles and straps.

A method to load stores on an aircraft, the method may be controlled by one or more controller and may include one or more acts of loading stores onto corresponding lift portions; determining a relative position of the aircraft; positioning the stores relative to the determined position of the aircraft; and securing the stores to corresponding hardpoints (HPs) of the aircraft.

A method to load stores on an aircraft, the method may be controlled by one or more controller and may include one or more acts of loading stores onto corresponding lift portions; determining a relative position of the aircraft; positioning the stores relative to the determined position of the aircraft; and securing the stores to corresponding hardpoints (HPs) of the aircraft.