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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. A COMPUTER CODE FOR FIRE PROTECTION AND RISK ANALYSIS OF NUCLEAR PLANTS.

    SBC: CFD Research Corporation            Topic: N/A

    THE PROPOSED RESEARCH IS TO ADVANCE THE STATE-OF-THE-ART OF DETERMINISTIC RISK ANALYSIS AND FIRE PROTECTION METHODOLOGY OF NUCLEAR POWER PLANTS. A COMPUTER CODE, BASED ON THE USE OF A FIELD (DISCRETIZATION) MODELING TECHNIQUE, WILL BE DEVELOPED THAT HAS SUFFICIENT FLEXIBILITY FOR ACCURATE/REALISTIC REPRESENTATIONS OF GEOMETRY, VENTILATION AND OTHER CONDITIONS PRESENT IN CABLE ROOMS AND CONTROL ROO ...

    SBIR Phase I 1987 Nuclear Regulatory Commission
  2. A RELIABLE, MECHANICAL CRYOCOOLER FOR 80 K COOLING IN SPACE

    SBC: Alabama Cryogenic Engineering, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1987 National Aeronautics and Space Administration
  3. HIGH SPATIAL RESOLUTION/LARGE FIELD OF VIEW DETECTOR AND DATA HANDLING SYSTEM FOR A SPACE BASED SOLAR VECTOR MAGNETOGRAPH

    SBC: Bgb Inc.            Topic: N/A

    N/A

    SBIR Phase I 1987 National Aeronautics and Space Administration
  4. IMPROVEMENTS IN THREE-DIMENSIONAL NAVIER-STOKES TWO-PHASE COMBUSTION COMPUTER MODELS

    SBC: Cham Of North America Inc            Topic: N/A

    THE OBJECTIVE OF THIS PROPOSAL IS TO IMPROVE THE EXISTING REFLAN3D-SPRAY COMPUTER CODE TO PROVIDE A STATE-OF-THE-ART MODEL FOR SIMULATING ROCKET THRUST CHAMBERS. THREE MAJOR AREAS OF IMPROVEMENT ARE PROPOSED: (A) ACCURACY; (B) PHYSICAL REALISM; AND (C) COMPUTATIONAL EFFICIENCY. THEIMPROVED PHYSICAL MODELS TO BE INCORPORATED ARE: TRANSIENT CAPABILITIES, CONJUGATE HEAT TRANSFER IN COMBUSTION COOLING ...

    SBIR Phase I 1987 National Aeronautics and Space Administration
  5. A COUPLED JET EMBEDDING AND EULERIAN-LAGRANGIAN APPROACH TO SIMULATE REACTIVE FLUID MECHANICS IN LIQUID ROCKET ENGINES

    SBC: Cham Of North America Inc            Topic: N/A

    AN ANALYTICAL MODEL AND A COMPUTER CODE FOR THE DETAILED SIMULATION OF THREE-PHASE FLOWS IN LIQUID ROCKET THRUST CHAMBERS IS PROPOSED. THE MODEL DESCRIBES BEHAVIOR OF THE LIQUID, DISPERSED AND GASEOUS PHASES IN A MOST EFFICIENT FORM. THE CONTINOUS GAS-PHASE FLOW AND COMBUSTION ARE DESCRIBED IN EULERIAN COORDINATES; THE SPRAY FLOW, DROPLET EVAPORATION AND COMBUSTION PROCESSES ARE SIMULATED IN A GRI ...

    SBIR Phase I 1987 National Aeronautics and Space Administration
  6. CONTROL OF MANUAL ENTRY ACCURACY IN MANAGEMENT/ENGINEERING INFORMATION SYSTEMS

    SBC: Gamma Research Inc.            Topic: N/A

    N/A

    SBIR Phase I 1987 National Aeronautics and Space Administration
  7. FEASIBILITY STUDY OF A NEXT GENERATION VPPA WELDING CONTROL SYSTEM

    SBC: General Digital Industries Inc            Topic: N/A

    NEW APPROACHES TO AUTOMATIC CONTROL ARE NEEDED IF VARIABLE POLARITY PLASMA ARC (VPPA) WELDING IS TO REALIZE ITS FULL POTENTIAL AS A RELIABLE, REPEATABLE, COST EFFECTIVE PROCESS.PRESENT VPPA CONTROL SYSTEMS ARE FIRST GENERATION, ELEMENTARY COMPUTER-BASED SYSTEMS THAT DEPEND ON PROGRAMS WHICH ARE EXPERIMENTALLY DERIVED, AND DO NOT COMPENSATE FOR ANOMOLIES INJECTED BY TOOLING, PART, AND OTHER INDEPEN ...

    SBIR Phase II 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. DEVELOPMENT OF GENERALIZED COMMUNICATIONS MODELS BY COMPOSITION FROM MODULES

    SBC: Pritsker Corp.            Topic: N/A

    ONE PROMISING APPROACH TO THE DEVELOPMENT OF GENERALIZED MODELS OF COMMUNICATION SYSTEMS IS COMPOSITION OF MODELS FROM COMPONENT MODEL MODULES. IN THIS APPROACH, MODELS OF INDIVIDUAL SYSTEM COMPONENTS ARE DEVELOPED AND SUBSEQUENTLY LINKED INTO A MODEL BY MODEL COMPOSITION SOFTWARE. AN INTEGRATED SOFTWARE ENVIRONMENT SUPPORTS THIS TECHNOLOGY BY MANAGING A MODELBASE OF MODEL MODULES PROVIDING FOR TH ...

    SBIR Phase I 1987 National Aeronautics and Space Administration
  10. SPACE-BASED SOLAR WATER HEATER

    SBC: Remtech Inc.            Topic: N/A

    MANNED SPACECRAFT ON LONG MISSIONS OR PERMANENTLY IN ORBIT (E.G. SPACE STATION) WILL REQUIRE HOT WATER FOR HOUSEKEEPINGCHORES SUCH AS CLOTHES AND DISH WASHING AND BATHING. THE ECLS SYSTEM WILL ALSO REQUIRE SIGNIFICANT AMOUNTS OF HOT WATER. IF THIS WATER IS ELECTRICALLY HEATED, MANY ADDITIONAL SQUARE FEET OF THE PHOTOVOLTAIC (PV) ARRAY WILL BE NEEDED. AN ATTRACTIVE ALTERNATIVE IS TO MOUNT A SOLAR C ...

    SBIR Phase II 1987 National Aeronautics and Space Administration

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