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  • Center Of Gravity Determination Apparatus For Fixed Wing Aerial Systems | TechLink
    learning more about this patent and related research and licensing opportunities please contact any of our Tech Managers at http techlinkcenter org about staff Patent Identifier 9026350 Status Active Categories Aerospace A Center of Gravity Determination Apparatus for Fixed Wing Aerial Systems NC 102046 comprising a lifting support structure designed to support a fixed wing aerial system FWAS wherein the lifting support structure allows the FWAS to freely pitch a 3 D translation mechanism operatively coupled to the lifting support structure designed to precisely position the lifting support structure in the x axis y axis and z axis a base support structure operatively coupled to the 3 D translation mechanism designed to support other components at least one resting support structure operatively coupled to the base support structure designed to support the FWAS when the lifting support structure is not providing support to the FWAS and wherein the at least one resting support structure is designed to prevent the FWAS from pitching rolling or yawing when the lifting support structure is not providing support to the FWAS USPTO url http patft uspto gov netacgi nph Parser patentnumber 9026350 Facebook Twitter Google Plus LinkedIn Main menu Home Licensing Joint R D

    Original URL path: http://techlinkcenter.org/patents/9026350 (2016-02-09)
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  • Ground Surface Reconnaissance Projectile | TechLink
    Status Active Categories Aerospace A ground surface reconnaissance projectile includes a tube launched 60 mm inert mortar round which remotely relays reconnaissance and surveillance data back to an operator after it has landed and uprighted itself The types of collected data include for example visual imagery of the target area in 360 degrees acoustic target tracking and voice recognition infra red motion detection and magnetic field disturbance sensing USPTO url

    Original URL path: http://techlinkcenter.org/patents/9024238 (2016-02-09)
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  • Enhanced Stability Extended Range (Guidance Adaptable) 40 Mm Projectile | TechLink
    Aerospace A cartridge launched in an M203 M320 gun launcher device which cartridge has fins of 1 5 inches in length to insure flight stability without spinning the cartridge The non spin makes the cartridge capable of having a guidance navigation and control canard actuating system added between the body and nose The guidance navigation and control canard actuating system features now make the cartridge suitable for successfully attacking stationary

    Original URL path: http://techlinkcenter.org/patents/9021961 (2016-02-09)
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  • Method Of Generating Hydrogen From The Reaction Of Stabilized Aluminum Nanoparticles With Water And Method Of Forming Stabilized Aluminum Nanoparticles | TechLink
    org about staff Patent Identifier 9011572 Status Active Categories Aerospace A method of generating hydrogen gas from the reaction of stabilized aluminum nanoparticles with water is provided The stabilized aluminum nanoparticles are synthesized from decomposition of an alane precursor in the presence of a catalyst and an organic passivation agent and exhibit stability in air and solvents but are reactive with water The reaction of the aluminum nanoparticles with water

    Original URL path: http://techlinkcenter.org/patents/9011572 (2016-02-09)
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  • Ship Or Air Deployable Automated Buoy Refueling Station For Multiple Manned Or Unmanned Surface Vessels | TechLink
    A fueling system including a ship or air deployable automated fueling station and one or more sea surface water vessels The fueling station including a ballast arrangement to maintain an optimal freeboard for fueling the one or more water vessels the fueling station and the one or more water vessels including a communication arrangement for communications between the fueling station and the one or more water vessels The fueling station

    Original URL path: http://techlinkcenter.org/patents/8991447 (2016-02-09)
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  • High Burning Rate Tactical Solid Rocket Propellant, And Related Method | TechLink
    a composition for a high burning rate solid rocket propellant where the composition includes a binder compounded with a soluble energetic additive a metallic fuel and an oxidative fuel The resulting composition has a tactical Class 1 3 hazard rating and a linear regression rate that is substantially equivalent to a tactical Class 1 1 hazard rating obtainable using solid rocket propellants The composition may include a heat conducting element

    Original URL path: http://techlinkcenter.org/patents/8986473 (2016-02-09)
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  • Method Of Improved Distribution Over The Surface Of A Parachute Canopy | TechLink
    line of the suspension line system is attached to the skirt A pair of first line members is attached to the canopy the pair of first line members extending in a substantially radial direction away from the skirt towards a center of the canopy A first end of each line member in the pair of first line members is connected together to the suspension line at the skirt A first

    Original URL path: http://techlinkcenter.org/patents/8985520 (2016-02-09)
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  • Optical Orbital Debris Spotter | TechLink
    research and licensing opportunities please contact any of our Tech Managers at http techlinkcenter org about staff Patent Identifier 8976245 Status Active Categories Aerospace Photonics Sensors An orbital debris detection system positionable on a satellite launchable into an earth orbit includes a light source having a collimated light output a curved mirror for receiving the collimated light output and forming a light sheet outside the satellite and a scattered light detector for detecting a scattered light from the light sheet resulting from orbital debris intersecting the light sheet and scattering light toward the detector The system can provide damage attribution on a space vehicle whether it was just hit by a piece of debris data gathering for debris models time location approximate debris size direction of trajectory that are starved for information on small 1 cm debris pieces measuring density and distribution of predominantly small 1 cm orbital debris in a debris cloud e g a cloud that is the result of a satellite collision and monitoring the performance of orbital debris removal efforts that target small debris USPTO url http patft uspto gov netacgi nph Parser patentnumber 8976245 Facebook Twitter Google Plus LinkedIn Main menu Home Licensing Joint R

    Original URL path: http://techlinkcenter.org/patents/8976245 (2016-02-09)
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