A system for neutralization of a target aerial vehicle comprises one or more counter-attack unmanned aerial vehicles (UAVs) and an aerial vehicle capture countermeasure tethering the counter-attack UAV(s) to a structure or ground. The counter-attack UAV(s) are operable to capture and neutralize the target aerial vehicle with the aerial vehicle capture countermeasure (e.g., a net). The system can comprise an on-board aerial vehicle detection system, and/or an external aerial vehicle detection system each having at least one sensor configured to detect the target aerial vehicle while in flight. The counter-attack UAV(s) and the associated detection systems may be autonomously operated for detecting and neutralizing a target aerial vehicle. The aerial vehicle capture countermeasure can be moved from a stowed position to a deployed position in response to coordinated flight of the counter-attack UAV(s). Associated methods and systems are provided.

A system for neutralization of a target aerial vehicle comprises one or more counter-attack unmanned aerial vehicles (UAVs) and an aerial vehicle capture countermeasure tethering the counter-attack UAV(s) to a structure or ground. The counter-attack UAV(s) are operable to capture and neutralize the target aerial vehicle with the aerial vehicle capture countermeasure (e.g., a net). The system can comprise an on-board aerial vehicle detection system, and/or an external aerial vehicle detection system each having at least one sensor configured to detect the target aerial vehicle while in flight. The counter-attack UAV(s) and the associated detection systems may be autonomously operated for detecting and neutralizing a target aerial vehicle. The aerial vehicle capture countermeasure can be moved from a stowed position to a deployed position in response to coordinated flight of the counter-attack UAV(s). Associated methods and systems are provided.

Launch and/or recovery for unmanned aircraft and/or other payloads, including via parachute-assist, and associated systems and methods are disclosed. An example unmanned aerial vehicle (UAV) system includes a lift device, a parachute, and a capture line. The lift device includes a canister. The parachute is stowed in and deployable from the canister. The capture line is attached to the parachute and to a line control device. The capture line is configured to be engaged by a capture device located at an end of a wing of a UAV.

The present disclosure relates to a launch system and method. The launch system and method can include at least a preliminary accelerator tube system (PAT) that can be combined with a main accelerator tube system (MAT). The PAT alone or combined with the MAT can be used for launch of a vehicle for testing and/or for delivery of a payload.

A unmanned aerial vehicle (UAV) battery changing station includes a UAV landing area configured to support a UAV coupled to a first battery when the UAV is resting on the battery changing station, a movable battery storage unit including a holding station configured to store a second battery, and a battery replacement member configured to retrieve the second battery from the holding station and couple the second battery to the UAV. The movable battery storage unit is configured to permit the holding station to rotate about an axis of rotation.

Apparatus and methods for marine capture of an unmanned aerial vehicle (UAV) using water for braking and damping are described. An example capture device is for capturing a UAV aboard a marine vessel located in a body of water. The capture device includes a mounting frame and a capture frame. The mounting frame is configured to be coupled to the marine vessel. The capture frame is configured to be rotatably coupled to the mounting frame. The capture frame is rotatable relative to the mounting frame about an axis of rotation. The capture frame includes a braking member configured to be submerged in the body of water. The braking member is configured to oppose rotation of the capture frame relative to the mounting frame based on a braking force to be applied to the braking member by the body of water.

Apparatus and methods for marine capture of an unmanned aerial vehicle (UAV) using water for braking and damping are described. An example capture device is for capturing a UAV aboard a marine vessel located in a body of water. The capture device includes a mounting frame and a capture frame. The mounting frame is configured to be coupled to the marine vessel. The capture frame is configured to be rotatably coupled to the mounting frame. The capture frame is rotatable relative to the mounting frame about an axis of rotation. The capture frame includes a braking member configured to be submerged in the body of water. The braking member is configured to oppose rotation of the capture frame relative to the mounting frame based on a braking force to be applied to the braking member by the body of water.

A method of capturing an aerial vehicle comprises rotating a first blade of the aerial vehicle, the first blade coupled to a hub of the aerial vehicle and having a contour configured to facilitate entanglement of a payload line of a winch system around the aerial vehicle. The method further comprises contacting, by a leading edge of the first blade, the payload line of the winch system and pulling the payload line towards the hub of the aerial vehicle, wherein the payload line is pulled towards the hub as the first blade continues to rotate and wherein continued rotation of the first blade causes the payload line to be tangled around the hub of the aerial vehicle.

Hydrogen is delivered from a first location to a second location by an airship, such as a lighter-than-air ship. The hydrogen may be produced at the first location and the second location is where the hydrogen is needed. Once produced, the hydrogen is then loaded onto the airship. In one approach, a hydrogen storage compartment in the airship is filled with hydrogen. After the airship has arrived at the second location, the hydrogen is retrieved and may be stored at the second location for use as an energy source.

The present disclosure describes various systems, devices, and methods configured to retrieve a fixed-wing aircraft from free flight using a flexible capture member and a monopole assembly.