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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. Thermally Insulated Flexible Composite Cores for Aerospace Applications

    SBC: Infinite Materials & Products, Inc.            Topic: N/A

    Aerospace composite panels containing a core structure usually use an expanded honeycomb of either aluminum, NOMEX, or carbon fiber. These types of composite panels are often used as structure since the honey-comb core provides stiffness in the "Z" direction. However, they provide no thermal insulation value. Aerospace craft operating both inside and outside the earth's atmosphere experience envir ...

    SBIR Phase I 1997 Department of DefenseMissile Defense Agency
  2. Thermionic Nuclear Thermal Propulsion Bimodal Reactor

    SBC: Applied Sciences Inc.            Topic: N/A

    BIMODAL REACTORS FOR POWER AND PROPULSION HAVE LONG BEEN OF INTEREST FOR MISSIONS REQUIRINGS BOTH HIGH POWER AND LARGE DELTA-V; E.G., HIGH ALTITUDE, GEOSYNCHRONOUS AND PLANETARY MISSIONS. IT PROPULSIVE THRUST AND ELECTRIC POWER CAN BOTH BE SUPPLIED FROM THE SAME UNIT, A LARGE POTENTIAL SAVINGS CAN OCCUR. SUCH A REACTOR CAN BE DEVELOPED FROM A URANIUM CARBIDE FUELED THERMIONIC REACTOR WITH SINGLE C ...

    SBIR Phase I 1993 Department of DefenseMissile Defense Agency
  3. Ultrafine HfC/TaC for Rocket Thrusters

    SBC: MATERIALS MODIFICATIONS INC            Topic: N/A

    Liquid rocket engine performance can be dramatically improved by increasing the wall temperatures for operation concurrent with a reduction in the component weight. The bipropellant fuel combustion temperatures are between 3000 "approx" 3500 C. The conventional thrusters and exit nozzles made of niobium alloys have a maximum operating temperature limit of 1600 C. A regenerative cooling technolo ...

    SBIR Phase I 1996 Department of DefenseMissile Defense Agency
  4. Ultrafine SiC for Optical Mirrors

    SBC: MATERIALS MODIFICATIONS INC            Topic: N/A

    SiC has exceptionally high thermal conductivity and low linear expansion coefficient to resist thermal distortion, high elastic modulus to resist pressure and bowing distortion. It is lightweight and wear resistant. It also has excellent corrosion resistance and outstanding load bearing characteristics at elevated temperatures. Its hardness is only surpassed by diamond, CBN and boron carbide. As ...

    SBIR Phase I 1996 Department of DefenseMissile Defense Agency
  5. Ultra-high Dielectric Constant Dielectric Materials

    SBC: TPL, INC            Topic: N/A

    N/A

    SBIR Phase I 1993 Department of DefenseMissile Defense Agency
  6. Ultrahigh Quality, Single-Crystal Bulk Silicon Carbide

    SBC: INTRINSIC SEMICONDUCTOR CORP.            Topic: N/A

    Silicon carbide materials will revolutionize semiconductor devices for military and commercial markets. The material's wide bandgap, high electric field breakdown, high thermal conductivity give SiC capabilities that far exceed those of silicon or gallium arsenide. Despite significant progress in silicon carbide development, fundamental defects--most prominently micropipes--persist. If SiC is to s ...

    SBIR Phase I 1997 Department of DefenseMissile Defense Agency
  7. Ultra High Surface Area Aluminum Nanocomposite Powder for Solid Fuel Propellants

    SBC: SIGMA TECHNOLOGIES INTERNATIONAL GROUP, INC.            Topic: N/A

    N/A

    SBIR Phase I 1996 Department of DefenseMissile Defense Agency
  8. Ultrasmooth Finishing Of Optics

    SBC: MATERIALS MODIFICATIONS INC            Topic: N/A

    OPTICS USED IN SENSORS OR MISSILE SYSTEMS ARE MADE FROM SAPPHIRE, OR SILICON CARBIDE BECAUSE OF THEIR EXCELLENT OPTICAL OR INSULATING PROPERTIES, THEIR INERT, AND THEIR ABILITY TO RESIST HARSH ENVIRONMENTS. POLISHING SAPPHIRE BY MECHANICAL OR MECHANOCHEMICAL METHODS INDUCES RESIDUAL DAMAGE AND LIMITS THE OVERALL SURFACE ROUGHNESS (USUALLY AROUND 1 MICROINCH). THIS ROUGHNESS PRODUCES SCATTERING CEN ...

    SBIR Phase I 1993 Department of DefenseMissile Defense Agency
  9. Ultraspectral Imager

    SBC: KESTREL CORP            Topic: N/A

    This Phase I SBIR demonstrates the underlying technology required to construct an ultraspectral imager that has the ability to spectrally resolve molecular absorption lines while simultaneously creating a two dimensional spatial mapping. The proposed instrument will have a spectral resolution that is better than 2 cm-1 and two dimensional spatial resolution that exceeds 2 milliradian. Based on Fou ...

    SBIR Phase I 1996 Department of DefenseMissile Defense Agency
  10. WORK UNDERLOAD IN MODERN NPP CIBTRIK ROOMS

    SBC: UES INC            Topic: N/A

    N/A

    SBIR Phase I 1993 Nuclear Regulatory Commission
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