A hot air balloon steering system for steering a hot air balloon includes a hot air balloon that includes a basket. A stand unit is movably coupled to the basket. The stand unit abuts a support surface thereby facilitating the basket to be spaced from the support surface when the hot air balloon is not in flight. A sail unit is movably coupled to the basket. The sail unit captures air when the hot air balloon is in flight. Moreover, the sail unit steers the hot air balloon when the hot air balloon is in flight.

A method and system for separating and releasing component parts of a payload of a floating platform in response to a high collision probability is disclosed. The method includes, determining if an in-flight aircraft is within at least a safety zone associated with a floating platform, wherein the floating platform comprises releasably-coupled component parts; and activating, responsive to a determination that the in-flight aircraft is within at least the safety zone, a release mechanism, wherein the release mechanism is configured to uncouple the component parts.

A method and system for separating and releasing component parts of a payload of a floating platform in response to a high collision probability is disclosed. The method includes, determining if an in-flight aircraft is within at least a safety zone associated with a floating platform, wherein the floating platform comprises releasably-coupled component parts; and activating, responsive to a determination that the in-flight aircraft is within at least the safety zone, a release mechanism, wherein the release mechanism is configured to uncouple the component parts.

A laminated load ring for a balloon assembly includes a plurality of ring stacking units stacked one on top of the other. Each of the ring stacking units can include a main body having a central opening, a plurality of arms, and at least one weld line. The plurality of arms may each extend away from the main body around a circumference of the main body. The at least one weld line can be formed on the main body. The plurality of arms of the plurality of ring stacking units may be aligned with one another. The weld line of each of the plurality of ring stacking units may be offset from the weld line of a directly adjacent ring stacking unit in a direction extending around the circumference of the laminated load ring.

A laminated load ring for a balloon assembly includes a plurality of ring stacking units stacked one on top of the other. Each of the ring stacking units can include a main body having a central opening, a plurality of arms, and at least one weld line. The plurality of arms may each extend away from the main body around a circumference of the main body. The at least one weld line can be formed on the main body. The plurality of arms of the plurality of ring stacking units may be aligned with one another. The weld line of each of the plurality of ring stacking units may be offset from the weld line of a directly adjacent ring stacking unit in a direction extending around the circumference of the laminated load ring.

A method and system for separating and releasing component parts of a payload of a floating platform in response to a high collision probability is disclosed. The method includes, determining if an in-flight aircraft is within at least a safety zone associated with a floating platform, wherein the floating platform comprises releasably-coupled component parts; and activating, responsive to a determination that the in-flight aircraft is within at least the safety zone, a release mechanism, wherein the release mechanism is configured to uncouple the component parts.

A method and system for separating and releasing component parts of a payload of a floating platform in response to a high collision probability is disclosed. The method includes, determining if an in-flight aircraft is within at least a safety zone associated with a floating platform, wherein the floating platform comprises releasably-coupled component parts; and activating, responsive to a determination that the in-flight aircraft is within at least the safety zone, a release mechanism, wherein the release mechanism is configured to uncouple the component parts.

Co-extruded and extruded high-altitude balloons and apparatus and methods for manufacture. A high-altitude balloon has a plurality of layers of coextruded balloon panel extrudate, a first one of the layers extrusion-bonded to a second one of the layers along a first edge, the second one of the layers extrusion-bonded to a third one of the layers along a strip spaced apart from the first edge, extrusion-bonding of successive layers alternating between the first edge and the strip, the first one of the layers and the last one of the layers extrusion-bonded together along a second edge.

An air monitoring device includes a main body defining a volume for receiving a gas and configured to move above a ground surface. The air monitoring device further includes a camera configured to detect image data corresponding to a surrounding environment of the main body. The air monitoring device further includes a power source configured to generate mechanical power to propel the main body through the surrounding environment. The air monitoring device further includes a network access device configured to communicate with a remote device. The air monitoring device further includes a processor configured to receive the image data and to cause the network access device to transmit the image data or processed data corresponding to the image data to the remote device.

An air monitoring device includes a main body defining a volume for receiving a gas and configured to move above a ground surface. The air monitoring device further includes a camera configured to detect image data corresponding to a surrounding environment of the main body. The air monitoring device further includes a power source configured to generate mechanical power to propel the main body through the surrounding environment. The air monitoring device further includes a network access device configured to communicate with a remote device. The air monitoring device further includes a processor configured to receive the image data and to cause the network access device to transmit the image data or processed data corresponding to the image data to the remote device.