High altitude reconnaissance vehicle
First Claim
1. A method of deploying an airship having un inflatable body, an airship payload and at least one propeller assembly comprising the steps of:
- packaging said airship in a compacted state for high altitude deployment as a missile payload within a missile;
flying said missile to a general area of deployment;
separating said missile payload from said missile at the general area of deployment;
boosting said separated missile payload to a predetermined location and a predetermined altitude;
releasing said airship from said boosted missile payload; and
deploying said airship at said predetermined location and predetermined altitude, wherein said deploying comprises the steps of;
inflating said inflatable body with one of a compressed gas and a chemically generated gas carried in said airship payload at a rate to maintain said predetermined altitude; and
deploying said at least one propeller assembly into an operational position for station keeping and relocating said airship, wherein said at least one propeller assembly is one of a foldable propeller assembly and an inflatable propeller assembly.
1 Assignment
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Accused Products
Abstract
An airship deployment system comprises an airship of unique shape having laminar flow over this shape to enable low power propulsion, capable remote control, comprising an inflatable body; a propeller assembly for station keeping and repositioning said airship and capable of being folded into a compacted position and unfolded into an operational position; and a payload, comprising gas for inflating said inflatable body; and means for transferring data between said airship and a remote location; and a missile for carrying said airship in a compacted state to a predetermined location and altitude, and releasing said airship at said predetermined location and altitude. When said airship is released from said missile said inflatable body is inflated and said propeller assembly is unfolded into said operational position.
52 Citations
25 Claims
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1. A method of deploying an airship having un inflatable body, an airship payload and at least one propeller assembly comprising the steps of:
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packaging said airship in a compacted state for high altitude deployment as a missile payload within a missile; flying said missile to a general area of deployment; separating said missile payload from said missile at the general area of deployment; boosting said separated missile payload to a predetermined location and a predetermined altitude; releasing said airship from said boosted missile payload; and deploying said airship at said predetermined location and predetermined altitude, wherein said deploying comprises the steps of; inflating said inflatable body with one of a compressed gas and a chemically generated gas carried in said airship payload at a rate to maintain said predetermined altitude; and deploying said at least one propeller assembly into an operational position for station keeping and relocating said airship, wherein said at least one propeller assembly is one of a foldable propeller assembly and an inflatable propeller assembly. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8)
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9. An airship deployment system comprising:
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an airship capable of remote control comprising; an inflatable body having a shape to achieve laminar flow; at least one propeller assembly, for station keeping and repositioning said airship, capable of being folded into a compacted position and unfolded into an operational position; and a payload, comprising; at least one of a chemically generated and compressed gas for inflating said inflatable body; and means for transferring data between said airship and at least one remote location; a missile payload having packaged therein said airship in a deflated and folded state; and a missile configured to retain and fly said missile payload to a general area of deployment and separate from said missile payload at said area of deployment, whereat said missile payload boosts itself to a predetermined location and predetermined altitude, whereat said missile payload releases said airship, wherein when said airship is released from said missile payload said inflatable body is inflated and said at least one propeller assembly is unfolded into said operational position. - View Dependent Claims (10, 11, 12, 13, 14, 15, 16)
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17. A high altitude reconnaissance Vehicle (HARVe) having an inflatable body, at least one foldable propeller assembly, and a payload, said payload comprising:
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a deployment module for controlling deployment of said HARVe a flight system module for controlling flight systems of said HARVe; a power module for providing and regenerating power for said HARVe; a communications module for providing data networking with another communications equipped HARVe; and a control unit for providing overall control of said HARVe, wherein said inflatable body is deflated and said at least one foldable propeller assembly is folded in a missile payload, said HARVe is released at a predetermined location and a predetermined altitude, said inflatable body is inflated, and said at least one foldable propeller assembly is unfolded, and wherein said inflatable body is made of a material that is ultra-violet cured by exposure to the sun once it is unfolded and inflated. - View Dependent Claims (18, 19, 20, 21, 22, 23, 24, 25)
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Specification