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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. MATERIALS AND PROCESSES FOR ASEROSPACE RTM

    SBC: Abaris            Topic: N/A

    THE U.S. AIR FORCE HAS AN INTEREST IN HIGH RATE, LOW COST, PRODUCTION PROCESSES FOR AIRCRAFT PARTS. ABARIS PROPOSES A COMBINED ANALYSIS AND TESTING PROJECT TO EXPLORE MODIFYING PRESENT RESIN TRANSFER MOLDING (RTM) TECHNIQUES TO EVALUATE THE FEASIBILITY OF THEIR USE IN THE PRODUCTION OF HIGH PERFORMANCE, AEROSPACE, COMPOSITE MATERIALS. EPOXY RESINS SHALL BE UTILIZED IN COMBINATION WITH GRAPHITE REI ...

    SBIR Phase I 1991 Department of DefenseAir Force
  2. NON CHROMATED CORROSION INHIBITORS FOR ADHESIVE BONDING AND PAINTING PROCESSES

    SBC: Advanced Material Systems            Topic: N/A

    THE USE OF TOXIC CHEMICALS DERIVED FROM METALS SUCH AS STRONTIUM, CALCIUM AND LEAD AS ANTI-CORROSIVES IN PAINT AND ADHESIVE BOND PRIMERS FOR ALUMINUN ALLOYS IS A WELL ESTABLISHED TECHNOLOGY. HOWEVER, USE OF CERTAIN TYPES OF "SURFACE ACTIVE AGENTS" SUCH AS ORGANO METALLIC COMPLEXES, QUATENARY CHELATING AGENTS AND GUANIDINES AND THEIR DERIVATIVES FOR CHEMICAL ANTICORROSION PURPOSES HAS REMAINED RELA ...

    SBIR Phase I 1991 Department of DefenseAir Force
  3. COMBUSTION PROCESSES IN SPACE STORABLE LIQUID ROCKET ENGINES

    SBC: Software & Engineering Associa            Topic: N/A

    THE EXHAUST FROM NTO/MMH FUEL RICH GAS GENERATORS (GG) ARE KNOWN TO CONTAIN A LARGE FRACTION OF AMMONIA. THIS PHENOMENON MAKES IT POSSIBLE TO ACTIVELY COOL A ROCKET NOZZLE WALL USING THE ENDOTHERMIC DECOMPOSITION OF AMMONIA. A REALISTIC ANALYSIS OF THIS COMBUSTION PROCESS IS TO BE DEVELOPED WHICH INCLUDES ROCKET NOZZLE FLOW WITH FINITE RATE CHEMICAL KINETICS AND THE TANGENTIAL SLOT INJECTION OF GG ...

    SBIR Phase II 1991 Department of DefenseAir Force
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