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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.

Displaying 1 - 10 of 90 results
 
  • Record 1 TO 90

  1. Wide-Angle Resonant Cavities for Superior Light Emitters

    SBC: PICOLIGHT, INC.            Topic: N/A

    N/A

    SBIR Phase I 1996 Department of DefenseMissile Defense Agency

  2. VOLTAGE TUNABLE MULTI-SPECTRAL INFRARED SENSOR

    SBC: Schmidt Instruments Inc.            Topic: N/A

    SCHMIDT INSTRUMENTS PROPOSES TO DEVELOP A NOVEL TUNABLE PHOTODETECTOR BASED ON A DOUBLE BARRIER PHOTON ASSISTED RESONANT TUNNELING STRUCTURE. THE DEVICE CAN BE FABRICATED FROM A NUMBER OF SEMICONDUCTOR SYSTEMS DEPENDING ON THE DETECTOR CHARACTERISTICS ONE DESIRES. FOR EXAMPLE, A DETECTOR BASED ON THE GAAS/ALGAAS SYSTEM WOULD BE CAPABLE OF DETECTING PHOTONS WITH ENERGIES THROUGHOUT THE INFRARED SPE ...

    SBIR Phase I 1991 Department of DefenseMissile Defense Agency

  3. VLSI-FLC LASER-BEAM STEERING DEVICE

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

    N/A

    SBIR Phase I 1991 Department of DefenseMissile Defense Agency

  4. VALIDATION & TESTING OF THE VAM2D COMPUTER CODE

    SBC: Hydrogeologic Inc.            Topic: N/A

    N/A

    SBIR Phase I 1988 Nuclear Regulatory Commission

  5. UNCOOLED INFRARED FOCAL PLANE ARRAYS BY USE OF NON-CONTACT ELECTRICAL INTERCONNECT

    SBC: Skw Corp            Topic: N/A

    N/A

    SBIR Phase I 1991 Department of DefenseMissile Defense Agency

  6. Ultra Low-Loss Optoelectronic Packaging

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

    Conventional optoelectronic packaging technologies failed to provide low-loss coupling among various optoelectronic devices that are pivotal for BMDO-mission-related tasks. To bridge different effective apertures of various optoelectronic devices are the major bottleneck needs to be overcome. Radiant Research, Inc., proposes a drastically new idea to solve this problem by introducing a mode-matche ...

    SBIR Phase I 1996 Department of DefenseMissile Defense Agency

  7. ULTRA-HIGH SPEED INCOHERENT-TO-COHERENT CONVERTER FOR OPTICAL COMPUTING

    SBC: Silicon Mountain Design, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1994 Department of DefenseMissile Defense Agency

  8. 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

  9. 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

  10. 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
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