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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. Advanced Cooling Techniques for Hydrocarbon Liquid Rocket Engine Components

    SBC: Software And Engineering Associates, Inc.            Topic: N/A

    Design of a high performance hydrocarbon liquid rocket engine (LRE) requires a thorough understanding of the heat transfer and cooling requirements of LRE's. An efficient cooling system is crucial in extending engine life and minimizing pumping power. Itis essential to be able to accurately calculate the thermal response to ensure that materials maintain structural integrity and the cooling chan ...

    SBIR Phase I 2003 Department of DefenseAir Force
  2. Advanced Injector Designs for Hydrocarbon Liquid Rocket Engine Components

    SBC: SIERRA ENGINEERING, INC.            Topic: N/A

    Combustion instability is one of the greatest development risks for liquid propellant engines. The risks arise in development of a stable injector design from a variety of sources - limited modelling capabilities, poor scalability and the high cost ofappropriate component test facilities. Sierra Engineering believes that much of the empirical data on the injection element's driving characteristic ...

    SBIR Phase I 2003 Department of DefenseAir Force
  3. COMBUSTION PROCESSES IN SPACE STORABLE LIQUID ROCKET ENGINES

    SBC: Software & Engineering Associa            Topic: N/A

    N/A

    SBIR Phase I 1990 Department of DefenseAir Force
  4. Controlling Aerodynamic Surface Flow with Nonthermal Plasma

    SBC: Atmospheric Glow Technologies            Topic: N/A

    The plasma surface flow controllers, or plasma actuators, are based on momentum transfer created by either locally accelerating the charged species of the plasma in the electric field or by globally accelerating the charged species of the plasma via aninduced traveling wave imposed by electric field generated by several phases of applied high voltage. Plasma based surface flow controllers have al ...

    SBIR Phase I 2003 Department of DefenseAir Force
  5. DEPTH POFILING IN ALGAAS AND LINOO3 USING SPUTTER INITIATED RESONANCE IONIZATION SPECTROSCOPY

    SBC: ATOM SCIENCES, INC.            Topic: N/A

    N/A

    SBIR Phase I 1983 Department of DefenseAir Force
  6. DETERMINATION OF EFFECTS OF INTEROPERABILITY ISSUES ON INTRATHEATER AIRLIFT

    SBC: AMERICAN METAL PROCESSING, INC.            Topic: N/A

    BETTER METHODS TO DELIVER AND DISSEMINATE CARGO ARE NECESSARY TO FULLY EXPLOIT THE CAPABILITIES OF FUTURE INTRATHEATER AIRLIFTERS. THE ARMY'S AND AIR FORCE RENEWED EMPHASIS ON MOBILITY WILL REQUIRE GREATER PRODUCTIVITY BY TRANSPORTATION RESOURCES TO ACHIEVE NATIONAL OBJECTIVES. THE NECESSITATES A MORE THOROUGHLY-INTEGRATED TRANSPORTATION NETWORK. ADVANCED TECHNOLGIES, MATERIALS, AND INNOVATIVE ENG ...

    SBIR Phase I 1990 Department of DefenseAir Force
  7. DEVELOPMENT OF SILICON CARBIDE METAL-SEMICONDUCTOR FIELD-EFFECT TRANSISTORS FOR HIGH POWER OPERATION AT HIGH TEMPERATURES

    SBC: CREE RESEARCH, INC.            Topic: N/A

    SILICON CARBIDE POSSESSES A UNIQUE COMBINATION OF PROPERTIES THAT ALLOW SIMULTANEOUS HIGH TEMPERATURE AND HIGH POWER OPERATION OF ELECTRONIC DEVICES MADE FROM THIS MATERIAL. THE CUBIC FORM OF SIC (BETA) HAS A WIDE BANDGAP (2.2 EV @ 27 DEG C), WHICH THEORETICALLY GIVES A MAXIMUM OPERABLE TEMPERATURE OF 925 DEG C. ALPHA SIC (6H) HAS AN EVEN WIDER BANDGAP OF 2.86 EV @ 27 DEG C, GIVING A MAXIMUM OPERA ...

    SBIR Phase II 1990 Department of DefenseAir Force
  8. EMERGING TECHNOLOGIES RESULTING IN LIGHTER AIRCRAFT WEIGHT INCREASED ENGINE PERFORMANCE (ISP) AND IMPROVED DESIGN TOOLS

    SBC: ACCURATE AUTOMATION CORPORATION            Topic: N/A

    N/A

    SBIR Phase I 1990 Department of DefenseAir Force
  9. Featherweight Displays (FWDs):Ultra-bright VCSEL-based, Full-color Microdisplays using Solderless Nanoscale Interconnects

    SBC: E-VIZ, INC.            Topic: N/A

    The Feather Weight Display is a novel design and integration of industrially mature technologies including ultra-density silicon circuits with ultra-dense chip-to-chip interconnections, ultra-density VCSEL arrays, nonlinear photonic upconverting colormaterials, and nonlinear optical elements. To demonstrate its potential is primarily a design process. Design of emissive and virtual retinal devic ...

    SBIR Phase I 2003 Department of DefenseAir Force
  10. Filter for Airborne Pathogens and Toxic Liquids

    SBC: ESPIN TECHNOLOGIES, INC.            Topic: N/A

    Recent terrorist activities have left virtually no question that futureprotection systems for warriors will need to address chemical-biologicalfiltration. Although filters are presently available for CB threat, thereremains a need for regenerating, signature-less filters that can trapnanoparticulates and biological pollutants. In this context, under Phase IeSpin proposes to provide a feasibility d ...

    SBIR Phase I 2003 Department of DefenseAir Force
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