[Federal Register Volume 61, Number 137 (Tuesday, July 16, 1996)]
[Notices]
[Pages 37092-37093]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 96-17969]


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NATIONAL AERONAUTICS AND SPACE ADMINISTRATION

[Notice 96-074]


Government-Owned Inventions; Available for Licensing

agency: National Aeronautics and Space Administration.

action: Notice of availability of inventions for licensing.

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summary: The inventions listed below are assigned to the National 
Aeronautics and Space Administration, have been filed in the United 
States Patent Trademark Office, and are available for licensing.
    Copies of patent applications cited are available from the Office 
of Patent Counsel, Ames Research Center. Claims are deleted from the 
patent applications to avoid premature disclosure.

date: July 16, 1996.

for further information contact: Ken Warsh, Patent Counsel, Ames 
Research Center, Mail Code 202A-3, Moffett Field, CA 94035; telephone 
(415) 604-5104, fax (415) 604-1592.
    NASA Case No. ARC-12,052-1GE: A Technique for the Areal Measurement 
of Surface Stress Vectors Using Liquid Crystal Coatings;
    NASA Case No. ARC-12,071-1GE: Source Doubles Diagraph Model 
Processing Method;
    NASA Case No. ARC-12,015-2GE: Image Data Compression Having Minimum 
Perceptual Error (Continuation in Part);
    NASA Case No. ARC-12,069-1GE: Environmentally Friendly Deicing 
Fluid;
    NASA Case No. ARC-12,011-2SB: Process to Prepare Uniform Low 
Density Structural Ceramic Alator System (Continuation in Part);
    NASA Case No. ARC-11,992-2GE: Rotorcraft Blade Vortex International 
Controller (Continuation in Part);
    NASA Case No. ARC-11,978-2SB: Flexible Ceramic Thermal Protection 
System Resistant to High Acoustic Noise (Continuation in Part);
    NASA Case No. ARC-14,008-1GE: Non Linear Wind Tunnel Modeling and 
Analysis Technology;
    NASA Case No. ARC-12,110-1LE: Wing Tip Fence for Reduction of Lift 
Generated Airframe Noise;
    NASA Case No. ARC-12,080-1GE: Temporal Resolution Process for 
Enhanced Visual Displays;
    NASA Case No. ARC-12,097-1LE: Hierarchical Network Management 
System;
    NASA Case No. ARC-12,072-1SB: Contactless Magnetic Slip Ring;
    NASA Case No. ARC-14,027-1GE: Hybrid Flexible and Rigid Ceramic 
Insulation;
    NASA Case No. ARC-14,057-1GE: Photonic Switching Device Using Light 
Bullets;
    NASA Case No. ARC-14,029-1SB: Surface Modification for Efficient 
Waterproofing;
    NASA Case No. ARC-14,063-1GE: Method and Apparatus for Monitoring 
of Daily Activity in Terms of Ground Reaction Forces;
    NASA Case No. ARC-11,890-2GE: Far Infrared Diffuses Refractor 
(Continuation in Part);
    NASA Case No. ARC-14,048-1GE: Autogenic Feedback Training;
    NASA Case No. ARC-14,030-1GE: Nose Cap Heat Shield;
    NASA Case No. ARC-14,031-1GE: Leading Edge Heat Shield 
Configuration for Vehicles During Atmospheric Entry at Hypersonic 
Speed;
    NASA Case No. ARC-14,043-1GE: Virtual Window for Vehicle Displays;
    NASA Case No. ARC-14,061-1GE: Viscoelastic Dovetail Damper for 
Rotor Blades;
    NASA Case No. ARC-12,092-1SB: Fiber Optic Lock;
    NASA Case No. ARC-12,099-1GE: Noise Reducing Screens for in Flow 
Pressure Sensors or Microphones;
    NASA Case No. ARC-12,069-2GE: Environmentally Friendly Anti Icing 
and Deicing Fluid (Continuation in Part);
    NASA Case No. ARC-069-3GE: Environmentally Friendly Anti Icing and 
Deicing Fluid (Foreign Filed Patent);
    NASA Case No. ARC-12,087-1SB: Ziconium Hafnaum Ceramic Composites 
for Enhanced Ablation Resistance;
    NASA Case No. ARC-12,081-1CU: Durable Advanced Flexible Reuseable 
Surface Insulation;
    NASA Case No. ARC-14,054-1GE: An Algorithum for Treating Systematic 
Errors in Data from Imaging Interferometers;

[[Page 37093]]

    NASA Case No. ARC-14,060-1LE: Blind Pointer;
    NASA Case No. ARC-14,051-1SB: Molded Structural Thermal Protection;
    NASA Case No. ARC-14,052-1SB: Integrated System Advanced Attachment 
Concept for Thermal Protection;
    NASA Case No. ARC-14,053-1LE: System and Method for Finite Element 
Simulation and Helicopter Turbulence.

    Dated: July 8, 1996.
Edward A. Frankle,
General Counsel.
[FR Doc. 96-17969 Filed 7-15-96; 8:45 am]
BILLING CODE 7510-01-M