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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. Computational Modeling of Coupled Acoustic and Combustion Phenomena Inherent to Gas Turbine Engines

    SBC: Flow Modeling and Simulation            Topic: AF131181

    ABSTRACT: Flow Modeling and Simulation, LLC (FMS), proposes to develop a computational software tool, herein designated AUG3D, that is intended to provide physics-based, multi-level, validated computational simulations of turbine engine component flow fields, particularly those associated with thrust augmentors, i.e., afterburners. This tool will be ideally suited for closely integrating physica ...

    SBIR Phase I 2013 Department of DefenseAir Force
  2. Replacement for Hexavalent Chromium Conversion Coatings for Magnesium and Zinc-Nickel

    SBC: METALAST INTERNATIONAL, INC.            Topic: AF083226

    The European Union''s RoHS and WEE Directives mandated the elimination of the carcinogenic, hexavalent chromium coatings for metals, including magnesium and zinc-nickel plated substrates.  The purpose of this project is to find chemistry that will meet requirements of industry performance specifications and of the mandate.  METALAST intends to explore trivalent chromium in conjunction with two o ...

    SBIR Phase I 2009 Department of DefenseAir Force
  3. Optical Switching Fabric

    SBC: OPTICOMP CORP.            Topic: AF083209

    The major requirements for this program include the modeling of optical switching fabric technologies appropriate to space-borne systems at very high speed. Specifically, this program will evaluate two OptiComp candidate optical transceiver technologies against a Serial Rapid IO switching fabric. A down-selection to one optical transceiver technology will be made. Then, a simulation of that Serial ...

    SBIR Phase I 2009 Department of DefenseAir Force
  4. Terabit Per Second Optical Router for Space-Based Satellite Network

    SBC: OPTICOMP CORP.            Topic: AF083191

    The major requirements for this program include the modeling of optical routing technologies appropriate to space-borne systems at very high speed. This program will investigate optical routing at speeds to from 3.125 ro 10 Gbps per channel, with a wavelength/channel density from 4 to 16 wavelengths. Models will be constructed for these regimes, and an experimental demonstration of an 8-wavelength ...

    SBIR Phase I 2009 Department of DefenseAir Force
  5. Novel Manufacturing Process of Optoelectronic Transceiver Technology

    SBC: OPTICOMP CORP.            Topic: AF083152

    The proposed program will develop OptiComp''s coarse WDM transceiver manufacturing technology.  This WDM optical transceiver technology is highly novel, emphasizing manufacturability, ruggedization, modularity, ease of upgrade and qualification, extensive built-in diagnostic monitoring and test capabilities, as well as superior performance with reduced manfacturing complexity.  The modular desig ...

    SBIR Phase I 2009 Department of DefenseAir Force
  6. Advanced Combustion Stability Analysis Tools for Ox-rich Preburners

    SBC: SIERRA ENGINEERING, INC.            Topic: AF083112

    The goal of this SBIR is the enhancement of the current state-of-the-art combustion instability analysis tools.  The planned enhancement is focused on capturing the effects of injection element distribution and the inclusion of substantial film cooling and diluent injection.  These characteristics are extremely important in the design of high-pressure oxygen rich staged combustion (ORSC) engines ...

    SBIR Phase I 2009 Department of DefenseAir Force
  7. 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
  8. High Channel Density Interconnect Modules for Air Platforms

    SBC: OPTICOMP CORP.            Topic: N/A

    The primary goal of the proposed Phase I SBIR effort is to develop high channel-density interconnect modules for use in air platforms. This will be accomplished using a unique, monolithic, WDM, optoelectronic module that has a high interconnect density,small form-factor, and is rugged enough to withstand harsh operating environments. OptiComp Corporation occupies a 7,000 square foot facility, wh ...

    SBIR Phase I 2003 Department of DefenseAir Force
  9. 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
  10. 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
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