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The Award database is continually updated throughout the year. As a result, data for FY19 is not expected to be complete until April, 2020.

  1. DEGRATION OF NUCLEAR PLANT TEMPERATURE SENSORS

    SBC: Analysis And Measurement Services Corporation            Topic: N/A

    SAFETY SYSTEM TEMPERATURE SENSORS IN NUCLEAR POWER PLANTS ARE SUBJECT TO PERFORMANCE DEGRATION BECAISE PF AGING EFFECTS. A PROGRAM OF LABORATORY TESTING AND IN-SITU TESTINGIS NEEDED TO ENSURE THAT AGING DOES NOT LEAD TO REDUCED SAFETY AND AVAILABILITY. MUCH OF THE TECHNOLOGY NEEDED FOR THIS PROGRAM NOW EXISTS AS ISOLATED METHODS AND PROCEDURES. THESE WILL BE USED IN THIS PROJECT TO PERFORM AN AGIN ...

    SBIR Phase II 1987 Nuclear Regulatory Commission
  2. DEVELOPMENT OF A THREE DIMENSIONAL VISION ALGORITHM FOR DIRECT TRANSFORMATION FROM IMAGE SPACE TO ROBOT JOINT SPACE

    SBC: Advanced Control Technologies            Topic: N/A

    A DIRECT TRANSFORMATION FROM IMAGE COORDINATES TO ROBOT JOINT COORDINATES WILL BE DEVELOPED TO SERVE AS THE BASIS FOR A BINARY VISION SYSTEM FOR SIX DEGREE OF FREEDOM ROBOT CONTROL. A SYSTEM IDENTIFICATION ALGORITHM WILL ENABLE THE SYSTEM TO BE USED AS A TURN-KEY SYSTEM WITH ANY ROBOT WHICH ACCEPTS JOINT COORDINATE INPUT. THE DIRECT TRANSFORMATION FROM IMAGE SPACE TO ROBOT JOINT SPACE WILL BE ACCO ...

    SBIR Phase I 1987 National Aeronautics and Space Administration
  3. SUPERSONIC COMBUSTION ENHANCEMENT BY A NONEQUILIBRIUM PLASMA JET

    SBC: Aerochem Research            Topic: N/A

    IT IS PROPOSED TO DETERMINE THE FEASIBILITY OF USING A NONEQUILIBRIUM PLASMA JET, DEVELOPED AT AEROCHEM OVER THE PAST QUARTER CENTURY, AS A MEANS OF ENHANCING IGNITION AND FLAME STABILIZATION IN AIR-BREATHING ENGINES AND IN SUPERSONIC COMBUSTION. SPECIFICALLY, WE WILL DETERMINE; IF IGNITION OF LEAN OR LOW PRESSURE MIXTURES CAN BE MADE MORE RELIABLE; IF FLAME HOLDING LIMITS CAN BE BROADENED, E.G., ...

    SBIR Phase I 1987 National Aeronautics and Space Administration
  4. AN ARBITRARY GRID CFD ALGORITHM FOR CONFIGURATION AERODYNAMICS

    SBC: Computational Mechan            Topic: N/A

    THIS PROPOSAL DESCRIBES A PROJECT TO DEVELOP AND EXAMINE A CFD NUMERICAL SOLUTION ALGORITHM FOR THE THREE-DIMENSIONAL EULER/NAVIER-STOKES EQUATIONS THAT DOES NOT RELY ON A WELL-STRUCTURED, BODY-FITTED COORDINATE SYSTEM FOR ROBUSTNESS. THE SPECIFIC APPLICATION IS FOR REALISTIC CONFIGURATION AERODYNAMICS ANALYSIS OF HIGH SPEED MIXED SUPERSONIC FLOWS AT LARGE REYNOLDS NUMBER. A THEORETICAL ANALYSIS F ...

    SBIR Phase II 1987 National Aeronautics and Space Administration
  5. ROTOR UNSTEADY AIRLOADS

    SBC: Continuum Dynamics Inc            Topic: N/A

    N/A

    SBIR Phase I 1987 National Aeronautics and Space Administration
  6. "DEVELOPMENT OF A UNIQUE LABORATORY STANDARD INDIUM GALLIUM ARSENIDE DETECTOR FOR THE 0.5-1.7 MICRON SPECTRAL RANGE "

    SBC: Eti Instrument Systems Inc.            Topic: N/A

    N/A

    SBIR Phase I 1987 National Aeronautics and Space Administration
  7. TUNABLE CW LASER FOR THE 1.08 MICRON REGION

    SBC: General Optronics Corp            Topic: N/A

    N/A

    SBIR Phase I 1987 National Aeronautics and Space Administration
  8. SIMULATION AND CONTROL OF FUTURE SPACECRAFT POWER SYSTEMS

    SBC: Krause P C & Associates Inc.            Topic: N/A

    RECENT TECHNICAL ADVANCEMENTS IN THE SEMICONDUCTOR DEVICE AND POWER CONDITIONING TECHNOLOGIES HAVE LED TO SUBSTANTIAL IMPROVEMENTS IN TERMS OF SIZE, WEIGHT, EFFICIENCY AND POWER QUALITY OF THE POWER CONDITIONING EQUIPMENT WHICH IS BEING CONSIDERED FOR SPACE APPLICATIONS. WITH THESE ADVANCEMENTS COMES AN ABUNDANCE OF DESIGN CHOICES AND INCREASED DEGREES OF FREEDOM WITH RESPECT TO POWER SYSTEM CONTR ...

    SBIR Phase I 1987 National Aeronautics and Space Administration
  9. INTELLIGENT GAS TUNGSTEN ARC WELDING CONTROL

    SBC: Mid-south Engineering, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1987 National Aeronautics and Space Administration
  10. AN EXTREME TEMPERATURE, ULTRACLEAN RADIANT FURNACE

    SBC: PRINCETON SCIENTIFIC INSTRUMENTS, INC.            Topic: N/A

    THIS IS A PROPOSAL TO DEVELOP A COOL-WALLED RADIANT FURNACE FOR OPERATION AT EXTREMELY HIGH TEMPERATURES (UP TO 3300 K IN THE PROTOTYPE VERSION OF THIS PROPOSAL). IT WILL EMPLOY REFRACTORY METAL ELECTRICAL RESISTANCE HEATERS IN CONFIGURATIONS THAT PRESENT NEAR ONE HUNDRED PERCENT VIEWFACTORS AS SEEN FROM THE OBJECT BEING HEATED. THE RADIANT FLUX TO THE WORKPIECE WILL BE EXTREMELY UNIFORM, PRODUCIN ...

    SBIR Phase I 1987 National Aeronautics and Space Administration

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