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Award Data

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The Award database is continually updated throughout the year. As a result, data for FY23 is not expected to be complete until September, 2024.

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. Composite Reinforcing Fiber and Interfacial Coating Process

    SBC: Sensintel Inc.            Topic: N/A

    N/A

    SBIR Phase I 1995 Department of DefenseAir Force
  2. Noninvasive Sensor for Measuring the Partial Pressure of Oxygen in Humans

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

    The air of this proposal is to develop a noninvasive probe that may be placed near, but not on, the patient or the patient's wound, to measure the partial pressure of dissolved oxygen in the interstitial body fluids. The sensor is capable of assessing gas pressure levels in a graduated fashion from superficial to deep, in both healthy and compromised tissues. The sensitivity is sufficient to mon ...

    SBIR Phase I 1995 Department of DefenseAir Force
  3. Turbulent Drag Reduction Using Sub-Acoustic Shell Modes

    SBC: APTEK, Inc.            Topic: N/A

    A versatile, low profile actuator for incrasing aircraft performance by decreasing frictional drag is proposed. The concept dcan completely internal to the aircraft, and requires no pats, orifices, or strutures extending into the flow field which may become fouled. The Phase I effort consists of a wind tunnel experiment to determine the range of operability of the actuator. An interim effort is al ...

    SBIR Phase II 1995 Department of DefenseAir Force
  4. Acoustic Monitor for Buried Structure Detection

    SBC: APTEK, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1995 Department of DefenseAir Force
  5. Phased Array Liquid Crystal Beamsteerer

    SBC: BOULDER NONLINEAR SYSTEMS, INC.            Topic: N/A

    N/A

    SBIR Phase I 1995 Department of DefenseAir Force
  6. A Massively Parallel Liquid Crystal Fourier Transform Spectrometer

    SBC: BOULDER NONLINEAR SYSTEMS, INC.            Topic: N/A

    N/A

    SBIR Phase I 1995 Department of DefenseAir Force
  7. Open Atmosphere In Situ Processing of Termal Control Thin Films for Spacecraft

    SBC: CCVD, Inc dba MicroCoating Technologies (MCT)            Topic: N/A

    Combustion chemical vapor deposition (CCVD), which was invented by the principal investigator, is the only open atmosphere CVD technique for ceramics and metals. The CCVD method has been shown to inexpensively and quickly apply dense, adherent, epitaxial thin films in a continuous manner. This technology can be used for the production of thermal control coatings onto spacecraft even after assemb ...

    SBIR Phase I 1995 Department of DefenseAir Force
  8. An Innovative All Solid-State Laser Source for Direct and Coherent Detection LIDAR

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

    N/A

    SBIR Phase I 1995 Department of DefenseAir Force
  9. A New Fabrication Technology for High-Toughnexx Ceramic Bearing Races for Advanced Turbine Engines

    SBC: Colorado Engrg Research Labora            Topic: N/A

    Ceramics offer higher temperature capability, lower density, and higher fatigue lifetimes compared to bearing steels. Low damage tolerance and fracture toughness of ceramics has eliminated their consideration for bearing raceways. Colorado Engineering Research Laboratory (CERL) is proposing a completely new fabrication technology to make Si*3*N*4* ceramic-matrix composite (CMC) bearing rings wit ...

    SBIR Phase I 1995 Department of DefenseAir Force
  10. Cryogenic Monopropellant for Advanced Rocket Propulsion

    SBC: CRYOCO, INC.            Topic: N/A

    All rocket propellant power derives from the reaction of a fuel and oxidizer. Accordingly, all liquid rockets, and especially all cryogenic liquid rockets, have two complete fuel systems. One set each of containment tanks, pumps, instrumentation, and so on. Solid rockets, on the other hand, have only one fuel system, so to speak. The solid rocket motor contains the fuel and oxidizer in a rubber-li ...

    SBIR Phase II 1995 Department of DefenseAir Force
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