Systems and applications of lighter-than-air (LTA) platforms
First Claim
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1. A system comprising:
- an airborne platform comprising a balloon comprising a gas enclosure, wherein the balloon is an unmanned balloon;
a GPS unit configured to determine geographic coordinates and velocities of the airborne platform;
a pressure sensor configured to determine an altitude of the airborne platform;
a processor, wherein the processor comprises an algorithm to determine whether to release a ballast based on a set of termination criteria;
a ballast release mechanism configured to release the ballast; and
a neck release mechanism configured to release a payload,wherein the system comprises a first flight termination device and a second flight termination device, wherein each of the first flight termination device and the second flight termination device is configured to cause termination of a flight of the airborne platform and has at least two power sources each configured to provide power to at least one of the first flight termination device and the second flight termination device.
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Abstract
Innovative new systems and method of operating the systems, wherein the system comprises an airborne platform comprising an unmanned balloon comprising a gas enclosure; a geographic locator or tracking system configured to determine geographical coordinates of the unmanned balloon; a payload comprising a transceiver, wherein the transceiver is capable of communicating with communication devices that are separate from the unmanned balloon; first and second flight-termination devices each configured to cause termination of a flight of the unmanned balloon; and at least two power sources each configured to provide power to at least one of the first and second flight-termination devices.
322 Citations
27 Claims
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1. A system comprising:
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an airborne platform comprising a balloon comprising a gas enclosure, wherein the balloon is an unmanned balloon; a GPS unit configured to determine geographic coordinates and velocities of the airborne platform; a pressure sensor configured to determine an altitude of the airborne platform; a processor, wherein the processor comprises an algorithm to determine whether to release a ballast based on a set of termination criteria; a ballast release mechanism configured to release the ballast; and a neck release mechanism configured to release a payload, wherein the system comprises a first flight termination device and a second flight termination device, wherein each of the first flight termination device and the second flight termination device is configured to cause termination of a flight of the airborne platform and has at least two power sources each configured to provide power to at least one of the first flight termination device and the second flight termination device. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17)
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18. A device comprising:
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two chambers to hold two different reactants; a metering pump; a reaction chamber; an electrically actuated valve; and a venting tube incorporated with a one-way valve, wherein the device is configured to release a ballast. - View Dependent Claims (19, 20, 21, 22, 23)
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24. A device comprising:
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two concentric tubes forming a neck connection wherein a top tube is attached to an airborne platform with a strap or a rubber band and fits within a bottom tube attached to a payload; a restraining mechanism for top tube to prevent from sliding out of the bottom tube by a monofilament line; a flexible seal to prevent gas from leaking at a junction formed from the top tube and the bottom tube, wherein the device is configured to release the payload from a balloon neck. - View Dependent Claims (25, 26)
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27. A system comprising an airborne platform comprising an unmanned balloon comprising a gas enclosure;
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a geographic locator or tracking system configured to determine geographical coordinates of the unmanned balloon; a payload comprising a transceiver, wherein the transceiver is capable of communicating with communication devices that are separate from the unmanned balloon; first and second flight-termination devices each configured to cause termination of a flight of the unmanned balloon; at least two power sources each configured to provide power to at least one of the first and second flight-termination devices; a payload release mechanism; and a recovery mechanism.
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Specification