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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.

Displaying 41 - 50 of 84 results
 
  • Record 1 TO 84

  1. SMART MATERIAL PRODUCTS FOR COMMUNICATION, SENSING AND ACTUATION

    SBC: LUNA INNOVATIONS INCORPORATED            Topic: N/A

    N/A

    SBIR Phase I 1996 National Aeronautics and Space Administration

  2. Lidar Systems For Atmospheric Measurements

    SBC: FIBERTEK, INC.            Topic: N/A

    N/A

    SBIR Phase I 1997 National Aeronautics and Space Administration

  3. TUNABLE SOLID-STATE UV FREQUENCY CONVERTER FOR OZONE DIAL INSTRUMENTATION

    SBC: FIBERTEK, INC.            Topic: N/A

    N/A

    SBIR Phase I 1996 National Aeronautics and Space Administration

  4. 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

  5. Transistion Control in Corner Flow of a Supersonic Square Nozzle

    SBC: High Technology Corporation            Topic: N/A

    "Quiet" (low-disturbance) wind tunnels, needed for transitionresearch, require cleverly designed nozzle contours forstabilization or delay of dominant instabilities in supersonicnozzle wall boundary layers. However, if a nozzle of squarecross-section

    SBIR Phase I 1994 National Aeronautics and Space Administration

  6. Drag-Prediction Algorithms for Navier-Stokes Solutions over Single- and Multi-Element Airfoils

    SBC: High Technology Corporation            Topic: N/A

    Accurate prediction of the aerodynamic lift and drag is acritical requirement in the development process of an aircraft.Presently, computational methods based on numerical solution ofthe Reynolds-averaged Navier-Stokes (N-S) equations are beingapplie

    SBIR Phase I 1994 National Aeronautics and Space Administration

  7. 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

  8. HYBRID LAMINAR FLOW CONTROL TECHNIQUE FOR ENGINE NACELLES

    SBC: High Technology Corporation            Topic: N/A

    N/A

    SBIR Phase I 1996 National Aeronautics and Space Administration

  9. A PROGRAMMING ENVIRONMENT FOR THE DEVELOPMENT OF LARGE SCIENTIFIC SYSTEMS ON A DISTRIBUTED COMPUTING NETWORK

    SBC: High Technology Corporation            Topic: N/A

    N/A

    SBIR Phase I 1996 National Aeronautics and Space Administration

  10. Active Suppression of Resonance Interactions between Shear-Layers and Cavities

    SBC: High Technology Corporation            Topic: N/A

    N/A

    SBIR Phase I 1994 National Aeronautics and Space Administration
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