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Award Data

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The Award database is continually updated throughout the year. As a result, data for FY24 is not expected to be complete until March, 2025.

Download all SBIR.gov award data either with award abstracts (290MB) or without award abstracts (65MB). A data dictionary and additional information is located on the Data Resource Page. Files are refreshed monthly.

The SBIR.gov award data files now contain the required fields to calculate award timeliness for individual awards or for an agency or branch. Additional information on calculating award timeliness is available on the Data Resource Page.

  1. ATMOSPHERIC AEROSOLS BY FT-IR"

    SBC: ADVANCED FUEL RESEARCH, INC.            Topic: N/A

    THE ATMOSPHERE CONTAINS MANY NATURALLY OCCURRING AND MANMADE FINE PARTICLES AND AEROSOLS. THESE PARTICLES AFFECTWEATHER, AIR QUALITY AND COMMUNICATIONS. KNOWLEDGE OF THEIRCONCENTRATION, COMPOSITION, DISTRIBUTION AND TRANSPORT IS IMPORTANT TO THE PREDICTION OF WEATHER, DETECTION AND CONTROL OF POLLUTION, HEALTH MONITORING OF VEGETATION AND ATMOSPHERIC CHEMISTRY. WHILE A METHODS PRESENTLY EXIST FOR ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
  2. THE ABILITY TO OPTIMIZE THE DESIGN OF V/STOL AIRCRAFT AND TOPREDICT THEIR PERFORMANCE REQUIRES A GOOD UNDERSTANDING OF THE COMPLEX JET-INDUCED PHENOMENA ASSOCIATED WITH THESE AIRCRAFT.

    SBC: Flow Research Inc            Topic: N/A

    THE ABILITY TO OPTIMIZE THE DESIGN OF V/STOL AIRCRAFT AND TOPREDICT THEIR PERFORMANCE REQUIRES A GOOD UNDERSTANDING OF THE COMPLEX JET-INDUCED PHENOMENA ASSOCIATED WITH THESE AIRCRAFT. PRESENTLY, EXPERIMENTAL WORK IS THE MAIN AVENUE FOLLOWED TO GAIN AN UNDERSTANDING OF V/STOL FLOWS. NUMERICAL SIMULATION HAS MANY ADVANTAGES NOT SHARED BY EXPERIMENTAL TOOLS. IT THEREFORE CAN COMPLEMENT EXPERIMENTAL ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
  3. THIS INVESTIGATION IS AIMED AT DEVELOPING AN ACTIVE FLOW CONTROL DEVICE TO GENERATE LARGE-SCALE, PERIODIC STRUCTURES IN A TURBULENT SHEAR FLOW.

    SBC: Flow Research Inc            Topic: N/A

    THIS INVESTIGATION IS AIMED AT DEVELOPING AN ACTIVE FLOW CONTROL DEVICE TO GENERATE LARGE-SCALE, PERIODIC STRUCTURES IN A TURBULENT SHEAR FLOW. THE DEVICE WILL BE USED ON AIRBORNE LASER PLATFORMS TO REDUCE OR ELIMINATE OPTICAL DISTORTION OF THE LASER BEAM CAUSED BY THE TURBULENCE. CONTROLLED EXPERIMENTS WILL BE CONDUCTED IN AN 18-METER TOWING TANK TO INVESTIGATE THE FEASIBILITY OF GENERATING LARGE ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
  4. RESEARCH TO INVESTIGATE THE POTENTIALS OF ABRASION JET IN TRANSPORT SYSTEMS CONSTRUCTION

    SBC: Fluidyne Corp            Topic: N/A

    HIGH-PRESSURE WATERJET IS ONE OF SEVERAL NEW METHODS FOR CUTTING MATERIALS DEVELOPED DURING THE LAST DECADE. CURRENTLY IT IS USED, AT STATIC WATER PRESSURE UP TO 60,000 PSI, TO CUT A WIDE VARIETY OF SOFT AND MEDIUM-HARD MATERIALS IN FACTORIES; IT HAS BEEN EVALUATED FOR GEOTECHNICAL APPLICATIONS WITH VERY LIMITED SUCCESS. THIS RESEARCH CONCERNS THE USE OF ABRASIVE-ENTRAINED WATERJET FOR CUTTING AND ...

    SBIR Phase II 1985 Department of Transportation
  5. IT IS PROPOSED TO SIMULATE ON THE COMPUTER, A SIX-PISTON, SELF-BALANCED STIRLING ENGINE.

    SBC: Martini Associates            Topic: N/A

    IT IS PROPOSED TO SIMULATE ON THE COMPUTER, A SIX-PISTON, SELF-BALANCED STIRLING ENGINE. THE DOUBLE-ACTING PISTONS ARE CONNECTED IN TWO RINGS OF THREE IN THE SIEMENS ARRANGEMENT USED IN MAY KINEMATIC STIRLING ENGINES. THE PISTONS WILL BE SUPPORTED BY A LEAF SPRING AND A BELLOWS AND SEALED BY THE BELLOWS. IF EXECUTED PROPERLY, THIS WILL RESULT IN LONG LIFE WITH NO SEAL FRICTION. BY USING A RING OF ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
  6. SME JOINTS AND COUPLING FOR ADVANCED COMPOSITE MATERIALS

    SBC: Memory Metals Inc.            Topic: N/A

    N/A

    SBIR Phase I 1985 National Aeronautics and Space Administration
  7. AN INVESTIGATION IS PROPOSED HEREIN TO FORMALIZE, TEST AND EVALUATE NEW TECHNIQUES FOR IMPROVING THE TRANSIENT ACCURACYOF IMPLICIT FINITE-DIFFERENCE ALGORITHMS FOR THE TWO AND THREE-DIMENSIONAL COMPRESSIBLE NAVIER-STOKES EQUATIONS.

    SBC: SCIENTIFIC RESEARCH ASSOC., INC.            Topic: N/A

    AN INVESTIGATION IS PROPOSED HEREIN TO FORMALIZE, TEST AND EVALUATE NEW TECHNIQUES FOR IMPROVING THE TRANSIENT ACCURACYOF IMPLICIT FINITE-DIFFERENCE ALGORITHMS FOR THE TWO AND THREE-DIMENSIONAL COMPRESSIBLE NAVIER-STOKES EQUATIONS. THEPROPOSED INVESTIGATION IS MOTIVATED BY THE NEED FOR COMPUTATIONAL METHODS OF IMPROVED ACCURACY AND EFFICIENCY FOR APPLICATION TO TRANSIENT MULTIDIMENSIONAL FLOWS IN ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
  8. VISCOUS COMPUTATIONAL ANALYSIS AND A CONSTRAINED OPTIMIZATION TECHNIQUE

    SBC: SCIENTIFIC RESEARCH ASSOC., INC.            Topic: N/A

    PROPER DUCT DESIGN IS A FUNDAMENTAL ENGINEERING PROBLEM WHICH CAN HAVE A MAJOR IMPACT UPON COMPNENT EFFICIENCY. CURRENT AEROSPACE APPLICATIONS, WHICH PLACE A PREMIUM ON COMPACT DESIGN AND CLOSELY FIT COMPONENTS, OFTEN EXACERBATE THIS PROBLEM. EXAMPLES ARE DUCTS ASSOCIATED WITH INLETS ANDNOZZLES AS WELL AS TRANSITION DUCTS BETWEEN ENGINE COMPONENTS. AT PRESENT TECHNOLOGY IS AVAILABLE TO COMPUTE THE ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
  9. A PROPOSAL IS PRESENTED HEREIN TO INITIATE A STUDY OF THE TRANSIENT BEHAVIOR OF A SILICON CHARGE COUPLED DEVICE (CCD) AND ITS RESPONSE TO INCIDENT RADIATION.

    SBC: SCIENTIFIC RESEARCH ASSOC., INC.            Topic: N/A

    A PROPOSAL IS PRESENTED HEREIN TO INITIATE A STUDY OF THE TRANSIENT BEHAVIOR OF A SILICON CHARGE COUPLED DEVICE (CCD) AND ITS RESPONSE TO INCIDENT RADIATION. THE MOTIVATION FOR THIS EFFORT IS BASED ON RECENT ANALYTICAL AND HARDWARE STUDIES WHICH HAVE IDENTIFIED THE POTENIALLY SIGNIFICANT BENEFITS I.E. REDUCED PSUEDONOISE (PN) CODE ACQUISITION TIME, THAT MAY BE ACHIEVED VIA THE APPLICATION OF CHARG ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
  10. PROPOSAL TO DEVELOP A NUMERICAL SIMULATION FOR THE INLET BUZZ PROBLEM BY SOLUTION OF THE TIME DEPENDENT NAVIER-STOKESEQUATIONS

    SBC: SCIENTIFIC RESEARCH ASSOC., INC.            Topic: N/A

    N/A

    SBIR Phase I 1985 National Aeronautics and Space Administration
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