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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. Wide-Range High-Boost Turbocharging System Using Advanced Aerodynamic Design Features

    SBC: Concepts NREC, LLC            Topic: 14d

    Increasingly stringent exhaust emissions and fuel economy legislation is forcing automotive engine designers to: 1) demand increased pressure ratios from turbocharger compressors to ensure complete fuel combustion, 2) use Exhaust Gas Recirculation for emission reduction, and 3) reduce engine displacement while maintaining or even increasing output power to reduce fuel consumption. These three chan ...

    SBIR Phase II 2018 Department of Energy
  2. Magnetic Bearings for Supercritical CO2 Service

    SBC: Concepts NREC, LLC            Topic: 29f

    The technology development for the supercritical CO2 (sCO2) power plant is well underway, and the first pilot plants are now under construction. The new pilot plants are sized for a 10 MW net power output; a good size to gain valuable data for larger utility scale power plants. This is also a very good size for the smaller, distributed power applications. The distributed power application is envis ...

    SBIR Phase II 2018 Department of Energy
  3. A Novel Integrated Low Leakage IPS and Thrust Bearing for Rocket Turbopumps

    SBC: Concepts NREC, LLC            Topic: AF181031

    A novel integrated inter-propellant seal and thrust bearing (IPS/TB) for rocket turbopump applications that uses the latest technology developments in seal coatings and additive manufacturing to advance the state-of-the-art. The IPS/TB has low propellant loss, requires little or no purge gas, and no continuous purge when the turbopump is not in operation. The thrust bearing portion can handle all ...

    SBIR Phase I 2018 Department of DefenseAir Force
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