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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. Light Weight Spherical Cryotank

    SBC: GLOYER-TAYLOR LABORATORIES INC            Topic: H204

    BHL? technology offers the means to reduce the mass of cryogenic propellant tanks by 75% relative to state-of-the-art metal tanks. Since propellant tanks are generally the largest individual mass item on a launch vehicle or spacecraft, this mass savings of this magnitude can have profound effect on vehicle performance. A conceptual design of a spherical BHL cryotank for the NASA Morpheus Lander ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  2. 3D Flow Field Measurements using Aerosol Correlation Velocimetry

    SBC: AeroMancer Technologies Corporation            Topic: A108

    AeroMancer Technologies proposes to develop a 3D Global Lidar Airspeed Sensor (3D-LGAS) using Aerosol Correlation Velocimetry for standoff sensing of high-resolution spatially and temporally resolved three-component global airspeeds using a scanning elastic lidar. The proposed instrument uses range-resolved elastic backscatter data from a scanning lidar beam to generate a 3D map of aerosol density ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  3. Hypersonic Neurocontrol Actuator and Testbed

    SBC: ACCURATE AUTOMATION CORPORATION            Topic: N/A

    The purpose of this proposal is to develop a new generation of "SMART" neurocontrol actuator system for use on Hypersonic aircraft. Develop a testbed to validate that the actuator system will work. This will also optimize and scale the testbed vehicle sizing. This concept using adaptive neural network technology will improve performance and behavior for Hypersonic aircraft like the National AeroSp ...

    SBIR Phase II 1995 National Aeronautics and Space Administration
  4. EMBEDDED PAVEMENT STRESS SENSORS CONTAINING PIEZOELECTRIC COMPOSITES

    SBC: Fiber Materials, Inc.            Topic: N/A

    FIBER MATERIALS, INC. (FMI) PROPOSES SENSORS WHICH CAN BE EMBEDDED IN PAVEMENT TO MEASURE STRESS AND STRAIN FROM TRUCKS PASSING OVER AT SPEEDS UP TO 60 MPH. THESE SIMPLE, DURABLE SENSORS WILL BE MADE FROM PIEZOELECTRIC COMPOSITES WHICH ACT AS PASSIVE SENSORS AND DEVELOP A CHARGE PROPORTIONAL TO THE APPLIED PRESSURE. THE CHARGE IS CONVERTED TO A VOLTAGE WHICH IS RECORDED ON NEARBY EQUIPMENT. THE PH ...

    SBIR Phase II 1995 Department of Transportation
  5. Lightweight Ceramic Ablators

    SBC: Fiber Materials, Inc.            Topic: N/A

    Future atmospheric entry vehicles will require thermal protection materials/systems that are more durable, lower weight, combined with highly efficient protection from atmospheric heating. One low density material concept has been found to exhibit good ablation and in-depth thermal response under simulated entry conditions. This material is a low density carbon fiber reinforced carbon matrix with ...

    SBIR Phase II 1995 National Aeronautics and Space Administration
  6. AN ARBITRARY GRID CFD ALGORITHM FOR CONFIGURATION AERODYNAMICS

    SBC: Computational Mechan            Topic: N/A

    THIS PROPOSAL DESCRIBES A PROJECT TO DEVELOP AND EXAMINE A CFD NUMERICAL SOLUTION ALGORITHM FOR THE THREE-DIMENSIONAL EULER/NAVIER-STOKES EQUATIONS THAT DOES NOT RELY ON A WELL-STRUCTURED, BODY-FITTED COORDINATE SYSTEM FOR ROBUSTNESS. THE SPECIFIC APPLICATION IS FOR REALISTIC CONFIGURATION AERODYNAMICS ANALYSIS OF HIGH SPEED MIXED SUPERSONIC FLOWS AT LARGE REYNOLDS NUMBER. A THEORETICAL ANALYSIS F ...

    SBIR Phase II 1987 National Aeronautics and Space Administration
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