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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. TEMPERATURE SENSITIVE, VARIABLE AREA FLOW REGULATOR FOR JOULE-THOMSON NOZZLES

    SBC: General Pneumatics Corporation            Topic: N/A

    CRYOCOOLERS AND GAS LIQUEFIERS UTILIZE ISENTHALPIC EXPANSION OF COOLED GAS IN JOULE-THOMSON NOZZLES. TO EFFECTIVELY OPTIMIZE USAGE OF THE COMPRESSED GAS, A VARIABLE GAS MASS FLOW RATE IS NECESSARY. A HIGH FLOW RATE IS REQUIRED INITIALLY WITH A PROGRESSIVE REDUCTION AS THE DESIGN CONDITION IS ATTAINED AND INTERMITTENT FLOW THEREAFTER DEPENDING ON THE LOAD DEMAND. THIS PROJECT INCORPORATES INNOVATIV ...

    SBIR Phase II 1986 National Aeronautics and Space Administration
  2. COMPUTATION OF THE TIP VORTEX FLOW FIELD FOR ADVANCED PROPELLERS

    SBC: SCIENTIFIC RESEARCH ASSOC., INC.            Topic: N/A

    THE BLADE TIP VORTEX FLOW FIELD HAS A SIGNIFICANT IMPACT ON THE AERODYNAMIC PERFORMANCE AND ACOUSTIC CHARACTERISTICS OF AIRCRAFT PROPELLERS. THIS PROJECT INVOLVES COMPUTATION OF TIP VORTEX GENERATION PROCESS FOR ADVANCED PROPELLERS USING A FORWARD MACHING PROCEDURE. THE PROCEDURE WOULD BE USED TO COMPUTE COMPRESSIBLE HIGH SUBSONIC, HIGH REYNOLDS NUMBER TURBULENT FLOW FIELD ENCOUNTERED IN ADVANCED ...

    SBIR Phase II 1986 National Aeronautics and Space Administration
  3. INTERNAL FLUID MECHANICS OF LIQUID PROPELLANT ROCKET THRUST CHAMBERS

    SBC: SCIENTIFIC RESEARCH ASSOC., INC.            Topic: N/A

    THIS PROJECT ADDRESSES A COMPUTER CODE CAPABLE OF ACCURATELY SIMULATING THE INTERNAL FLUID MECHANICS OF LIQUID PROPELLANT ROCKET THRUST CHAMBERS USING A COMBINED EULERIAN-LAGRANGIAN DESCRIPTION. SUCH A CODE WILL BE EXTREMELY USEFUL IN CONDUCTING A PARAMETRIC STUDY OF THE EFFECT OF DESIGN PARAMETERS ON ENGINE PERFORMANCE AND IN STUDYING THE PERFORMANCE OF THRUST CHAMBERS WITH VARIABLE THRUST. WHILE ...

    SBIR Phase II 1986 National Aeronautics and Space Administration
  4. A COLOR SCHLIEREN SYSTEM FOR LARGE SCALE LOW-GRAVITY MPS FLUIDS EXPERIMENTS

    SBC: System Specialists, Inc.            Topic: N/A

    A NUMBER OF LOW GRAVITY MATERIALS PROCESSING EXPERIMENTS SUCH AS CRYSTAL GROWTH STUDIES REQUIRE A SPECIALIZED OPTICAL SYSTEM CAPABLE OF FLOW VISUALIZATION. SEVERAL SUCH SYSTEMS HAVE BEEN BUILT FOR USE IN SPACE AND BALLISTIC AIRCRAFT FLIGHTS, INCLUDING SCHLIEREN SYSTEMS. HOWEVER, NO COLOR SCHLIEREN SYSTEM HAS BEEN DEVELOPED FOR THESE APPLICATIONS. A COLOR SCHLIEREN SYSTEM PRODUCES DATA MORE AMENABL ...

    SBIR Phase II 1986 National Aeronautics and Space Administration
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