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Award Data

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The Award database is continually updated throughout the year. As a result, data for FY23 is not expected to be complete until September, 2024.

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.

Displaying 41 - 50 of 60 results
 
  • Record 1 TO 60

  1. A Novel Computational Tool For Hypersonic Transition Prediction

    SBC: High Technology Corporation            Topic: N/A

    N/A

    SBIR Phase I 1997 National Aeronautics and Space Administration

  2. DYNAMIC TESTING AND HIGH FIDELITY MODELING OF NONLINEAR UNSTEADY AERODYNAMICS

    SBC: BIHRLE APPLIED RESEARCH INC            Topic: N/A

    N/A

    SBIR Phase I 1996 National Aeronautics and Space Administration

  3. A Stand-Alone Sensitivity Solver For Hypersonic Design Applications

    SBC: AEROSOFT INC            Topic: N/A

    N/A

    SBIR Phase I 1997 National Aeronautics and Space Administration

  4. DAMPER- DIGITAL ACTIVE MATERIALS-PROCESSING PLATFORM EFFORT

    SBC: A-TECH CORPORATION            Topic: N/A

    N/A

    SBIR Phase I 1988 National Aeronautics and Space Administration

  5. KENNEDY SPACE CENTER ATMOSPHERIC BOUNDARY LAYER EXPERIMENT

    SBC: ENSCO Inc            Topic: N/A

    N/A

    SBIR Phase I 1988 National Aeronautics and Space Administration

  6. NUMERICAL MODELING OF FULLY VISCOUS ROCKET PLUME FLOWS

    SBC: Gt-devices Inc            Topic: N/A

    THE PLUME PRODUCED BY THE GAS FLOW THROUGH THE NOZZLE OF A ROCKET ENGINE OR SYSTEM VENT ON A SPACECRAFT CAN CONTAMINATETHE SPACECRAFT, ITS SENSORS AND OTHER NEARBY APPARATUS. ANALYTIC METHODS FAIL FOR DENSE OR COOL EXHAUST GAS, WHICH EXHIBITS VISCOUS BOUNDARY LAYER FLOW, AND NUMERIC SOLUTIONS FOR THE NOZZLE CORE FLOW ARE THEN PATCHED TO THOSE FOR THE BOUNDARY LAYER FLOW. THE RESULTING CONTINUUM SO ...

    SBIR Phase I 1988 National Aeronautics and Space Administration

  7. VALIDATION & TESTING OF THE VAM2D COMPUTER CODE

    SBC: Hydrogeologic Inc.            Topic: N/A

    N/A

    SBIR Phase I 1988 Nuclear Regulatory Commission

  8. FORCE REFLECTING JOYSTICKS FOR MANIPULATOR CONTROL

    SBC: Meridian Corp.            Topic: N/A

    N/A

    SBIR Phase I 1988 National Aeronautics and Space Administration

  9. MICRO COMPUTER BASED PARALLEL PROCESSING SYSTEM FOR CODE COMPUTATIONS

    SBC: Risk Management Systems            Topic: N/A

    N/A

    SBIR Phase I 1988 Nuclear Regulatory Commission

  10. MINIATURIZED TANDEM MASS SPECTROMETER FOR MANNED SPACE MISSIONS

    SBC: Viking Instruments Corp.            Topic: N/A

    N/A

    SBIR Phase I 1988 National Aeronautics and Space Administration
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