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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. Fault-to-Failure Progression Modeling of Propulsion System and Drive Train Bearings for Prognostic and Useful Performance Life Remaining Predictions

    SBC: SENTIENT SCIENCE CORPORATION            Topic: N02195

    Military and commercial aircraft operators are moving toward predictive maintenance to minimize costs while maximizing asset availability and safety. Key technological prerequisites for this new approach are the ability to monitor the condition of critical components, and the ability to accurately forecast their remaining useful life. Phase I of this project clearly demonstrated the feasibility of ...

    SBIR Phase II 2004 Department of DefenseNavy
  2. Featherweight Displays (FWDs):Ultra-bright VCSEL-based, Full-color Microdisplays using Solderless Nanoscale Interconnects

    SBC: E-VIZ, INC.            Topic: AF03069

    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 color materials, and nonlinear optical elements. To demonstrate its potential is primarily a design process. Design of emissive and virtual retinal devi ...

    SBIR Phase II 2004 Department of DefenseAir Force
  3. Carbon Foam Composite Tooling

    SBC: TOUCHSTONE RESEARCH LABORATORY, LTD.            Topic: MDA03049

    Touchstone Research Laboratory has developed a novel material, CFOAMr. The primary enabling carbon foam characteristic is that the Coefficient of Thermal Expansion (CTE) values are comparable to carbon fiber polymer matrix systems in manufacturing advanced composites. Other advantages of carbon foam-based tools are low mass, reduced energy, easy modifications, unmatched repair capabilities, and r ...

    SBIR Phase II 2004 Department of DefenseMissile Defense Agency
  4. Advanced Injector Designs for Hydrocarbon Liquid Rocket Engine Components

    SBC: SIERRA ENGINEERING, INC.            Topic: OSD03010

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

    SBIR Phase II 2004 Department of DefenseAir Force
  5. Distributed Optoelectronic Crossbar Modules for Backplane Applications

    SBC: OPTICOMP CORP.            Topic: BMDO00011

    The primary goal of the proposed Phase II effort is to develop monolithic distributed optoelectronic crossbar modules for implementation of high performance distributed crossbar backplanes. The high density monolithic crossbar modules will enable distributed backplane architectures that are highly scalable. In addition, the distributed crossbar modules will provide backplanes that are high speed ...

    SBIR Phase II 2004 Department of DefenseMissile Defense Agency
  6. Coal-Based Porous Graphite for Aerospace Heat Exchanger Applications

    SBC: TOUCHSTONE RESEARCH LABORATORY, LTD.            Topic: AF03118

    A newly developed "coal-based" porous graphite material has been recently produced. This development is a direct result of Touchstone Research Laboratory's Phase I funding to develop enhanced-strength carbon foam heat-exchanger materials for aerospace applications since low density carbon foams cannot endure high bleed air pressures in aerospace pre-coolers and heat exchangers. The newly develope ...

    SBIR Phase II 2004 Department of DefenseAir Force
  7. Monolithic WDM Technology for Integrated Vehicle/Mission Management Systems

    SBC: OPTICOMP CORP.            Topic: AF03235

    Optoelectronic technologies make it possible to construct systems that are tolerant to the unique threats of aerospace environments. The goal of this proposed Phase II effort is to develop, fabricate, and demonstrate OptiComp Corporation's (OCC) WDM optoelectronic transmitter and receiver technologies for connection sensors with the vehicle and mission management computer systems. Working with B ...

    SBIR Phase II 2004 Department of DefenseAir Force
  8. Optimal Bioaerosol Sampler

    SBC: MANNING APPLIED TECHNOLOGY            Topic: ARMY03T20

    Development of an Optimal Bioaerosol Sampler with enhanced optical triggering capability is proposed, following a highly successful Phase I effort that clearly demonstrated feasibility. The threat of a bioaerosol attack can be partially mitigated by deployment of a cost-effective sensor network. High priority programs, such as BioWatch and Portal Shield will benefit from a sensor compliant to Join ...

    STTR Phase II 2004 Department of DefenseArmy
  9. Future Technology for Aerospace Structures Technology

    SBC: FMW COMPOSITE SYSTEMS, INC.            Topic: AF03237

    The continued development of hypersonic vehicles and high performance space access vehicles has highlighted the importance of light-weight, load-bearing structures capable of prolonged exposure at elevated temperatures. The optimal solution to this problem would be a hot primary structure capable of supporting the required loads at elevated temperature while also providing the necessary thermal pr ...

    SBIR Phase II 2004 Department of DefenseAir Force
  10. Advanced Cooling Techniques for Hydrocarbon Liquid Rocket Engine Components

    SBC: Software And Engineering Associates, Inc.            Topic: OSD03009

    Liquid rocket engines may be run for repeatedly over extended periods of time, requiring active cooling. An efficient means of cooling LRE nozzles involves using the liquid fuel or oxidizer itself to provide the cooling, often referred to as regenerative cooling. SEA's liquid rocket combustion chamber and nozzle design code, TDK, can predict the heat transfer to the surface of the nozzle as a fu ...

    SBIR Phase II 2004 Department of DefenseAir Force
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