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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. SPACE CRAFTS

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

    A METHODOLOGY FOR ANALYZING TWO-PHASE FLOW SYSTEM IN A MICROGRAVITY ENVIRONMENT WILL BE DEVELOPED. THE MAIN OBJECTIVE OF THIS PROPOSAL IS TO CONSTRUCT A COMPUTER MODEL WHICH WILL BE HELPFUL IN THE EVALUATION OF COMCEPTUAL DESIGNS OF THERMAL CONDITIONING SYSTEMS FOR SPACE CRAFTS. THE MIDEL WILL ALSO PROVIDE A TOOL FOR ANALYZING TRANSIENTS DUE TO START UP, SHUTDOWN OR ACCIDENTAL SITUATION. ONE OF TH ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
  2. FEASIBILITY STUDY OF A NEXT GENERATION VPPA WELDING CONTROL SYSTEM

    SBC: General Digital Industries Inc            Topic: N/A

    N/A

    SBIR Phase I 1985 National Aeronautics and Space Administration
  3. SYSTEM

    SBC: Nichols Research Corp            Topic: N/A

    THE PROPOSED INNOVATIVE RESEARCH IS TO DESIGN AND DEVELOP THE ARTIFICIAL INTELLIGENCE (AI) COMPONENTS NEEDED TO CREATEA DEDUCTIVELY AUGMENTED NASA MANAGEMENT DECISION SUPPORT SYSTEM (DANMDS). PHASE I OF THE RESEARCH EFFORT WILL IDENTIFY THE AI COMPONENTS REQUIRED FOR SUPPORTING NATURAL LANGUAGE INTERFACE, DECISION-SUPPORT RULE BASE DEVELOPMENT, APPROPRIATE KNOWLEDGE REPRESENTATION SCHEMA AND SEARC ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
  4. THE LOW EARTH ORBIT SPACE STATION WILL PRODUCE A LOCAL GAS CLOUD AND RESULTING CONTAMINATION GENERATED BY (1) OUTGASSING FROM NONMETALLIC MATERIALS, (2) EARLY DESORPTION FROM EXTERNAL SURFACES, (3) LEAKAGE OF THE CABIN ATMOSPHERE,(4) VENTING OF

    SBC: Remtech Inc.            Topic: N/A

    THE LOW EARTH ORBIT SPACE STATION WILL PRODUCE A LOCAL GAS CLOUD AND RESULTING CONTAMINATION GENERATED BY (1) OUTGASSING FROM NONMETALLIC MATERIALS, (2) EARLY DESORPTION FROM EXTERNAL SURFACES, (3) LEAKAGE OF THE CABIN ATMOSPHERE,(4) VENTING OF CONDESNATES, AND (5) REACTION CONTROL PLUMES.THIS VERY LOW DENSITY GAS FLOW IS BEST MODELED USING MONTE CARLO METHODS. THE KEY TO USEFUL ENGINEERING PREDIC ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
  5. SPACE-BASED SOLAR WATER HEATER

    SBC: Remtech Inc.            Topic: N/A

    N/A

    SBIR Phase I 1985 National Aeronautics and Space Administration
  6. AERODYNAMIC HEATING UPGRADE OF THE PARABOLIZED NAVIER-STOKES(PNS) CODE

    SBC: Remtech Inc.            Topic: N/A

    N/A

    SBIR Phase I 1985 National Aeronautics and Space Administration
  7. THE OBJECTIVE OF THIS EFFORT IS TO DEVELOP AND EXAMINE THE THEORETICAL BASIS FOR IN SITU PARTICLE SIZING WITH A LASER DOPPLER VELOCIMETER-LDV OPTICAL SYSTEM.

    SBC: SRS Technologies            Topic: N/A

    THE OBJECTIVE OF THIS EFFORT IS TO DEVELOP AND EXAMINE THE THEORETICAL BASIS FOR IN SITU PARTICLE SIZING WITH A LASER DOPPLER VELOCIMETER-LDV OPTICAL SYSTEM. THE INNOVATION OF THE PROPOSED APPROACH IS THE SIMULTANEOUS MEASUREMENT OF FOUR DIFFERENT LDV SIGNAL CHARACTERISTICS TO OBTAIN SIMULTANEOUSLY AND IN SITU, PARTICLE SIZE DISTRIBUTIONS, PARTICLE NUMBER DENSITIES AND PARTICLE VELOCITIES, FOR PAR ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
  8. 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
  9. 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
  10. 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

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