An aircraft store ejector systems and subsystems thereof. Embodiments can include a two-reservoir re-pressurization system wherein a remote reservoir is used to maintain desired pressure in a local ejector reservoir. The system can include a release valve having a vent valve and valve piston. The release valve can control release of pressurized gas to a pitch control valve. The pitch control valve can be configured to distribute the pressurized gas between two or more ejector piston assemblies. One or more of the ejector piston assemblies can include multiple concentric piston stages and piston chambers, the piston chambers configured to contain a volume of gas. The ejector piston assemblies can be configured to compress the volume of gas within the piston chambers as the piston stages are extended out from the aircraft. Such compression can provide a return force to the piston stages.

A system and method for intelligently and dynamically deploying a plurality of mobile robotic machines capable of carrying out a complex series of actions automatically to propagate wireless network connectivity comprising, at least, a mechanical framework, sensors, actuators, communications capability, an energy source, a propulsion means, a control mechanism, and a payload. The payload may comprise electronic or mechanical communication equipment to propagate services such as wireless networking services, in for example, a first responder or emergency environment, or electronic and mechanical jamming services in a military or anti-terrorism environment.

Described is an aerial vehicle, such as an unmanned aerial vehicle (“UAV”) that includes a delivery shroud. The delivery shroud may be maintained in a retracted position while the aerial vehicle is in transit. The delivery shroud reduces the transmission of sound from the aerial vehicle to the delivery area. Likewise, the delivery shroud may also be used to facilitate delivery of a payload from the aerial vehicle to a delivery location within the delivery area.

An unmanned aerial vehicle system includes an unmanned aerial vehicle, a tether assembly selectively coupled to the unmanned aerial vehicle, a processor, and a memory. The memory contains instructions thereon, which, when executed by the processor, cause the system to disconnect the tether assembly from the unmanned aerial vehicle.

An unmanned aerial vehicle system includes an unmanned aerial vehicle, a tether assembly selectively coupled to the unmanned aerial vehicle, a processor, and a memory. The memory contains instructions thereon, which, when executed by the processor, cause the system to disconnect the tether assembly from the unmanned aerial vehicle.

A detachable connecting arrangement for fitting launchable external loads to an aircraft, having a hook-like connecting element fitted to the external load and a holding element fitted to the aircraft for the hook-like connecting element. The hook-like connecting element includes a lower supporting surface and an upper supporting surface. The holding element has a first opposing supporting surface that interacts with the lower supporting surface, and a second, upper opposing supporting surface that interacts with the upper supporting surface. The lower supporting surface and the first opposing supporting surface are designed to support mass forces of the external load directed away from the aircraft, and the upper supporting surface and the upper opposing supporting surface are designed to support mass forces of the external load directed towards the aircraft.

A detachable connecting arrangement for fitting launchable external loads to an aircraft, having a hook-like connecting element fitted to the external load and a holding element fitted to the aircraft for the hook-like connecting element. The hook-like connecting element includes a lower supporting surface and an upper supporting surface. The holding element has a first opposing supporting surface that interacts with the lower supporting surface, and a second, upper opposing supporting surface that interacts with the upper supporting surface. The lower supporting surface and the first opposing supporting surface are designed to support mass forces of the external load directed away from the aircraft, and the upper supporting surface and the upper opposing supporting surface are designed to support mass forces of the external load directed towards the aircraft.

In one embodiment, an apparatus includes a collapsible workstation assembly to be used in a temporarily-mounted control system of an aircraft. The collapsible workstation assembly is mounted to a floor of the aircraft via one or more mounting plates and one or more adaptive floor plates. The collapsible workstation assembly includes a number of modules for display and user controls. Each of the modules are connected via hinges and hinge locks to be moved between a deployed position for use and a stowed position when not in use. The collapsible workstation assembly is further connected to an observer chair assembly and a temporary door plug.

In one embodiment, an apparatus includes a collapsible workstation assembly to be used in a temporarily-mounted control system of an aircraft. The collapsible workstation assembly is mounted to a floor of the aircraft via one or more mounting plates and one or more adaptive floor plates. The collapsible workstation assembly includes a number of modules for display and user controls. Each of the modules are connected via hinges and hinge locks to be moved between a deployed position for use and a stowed position when not in use. The collapsible workstation assembly is further connected to an observer chair assembly and a temporary door plug.

Autonomous delivery drop points for delivery of an item are provided. The autonomous delivery drop points can include a proxy sensor to communicate information related to the autonomous delivery drop point to an autonomous delivery vehicle. The autonomous delivery drop points can include a delivery inlet configured to accept the item. The autonomous delivery drop points can include a storage receptacle configured to store the item until the item is retrieved by the owner of the item. The autonomous delivery drop points can include an attachment member coupled to the item. The autonomous delivery drop points can include a hook configured to couple to the attachment member to accept the item, wherein the hook comprises the proxy sensor.