Award Data

For best search results, use the search terms first and then apply the filters
Reset

The Award database is continually updated throughout the year. As a result, data for FY19 is not expected to be complete until June, 2020.

  1. Development of ZnO-GaN hybrid spin LED

    SBC: CERMET, INC.            Topic: AF03T020

    Cermet, Inc in collaboration with Georgia Institute of Technology proposes to develop spin Light Emitting Diode (LED) in a 24 month Phase II program. The spin LED is a simple yet powerful spintronic device that produces circularly polarized light and is a potent tool to quantify the spin injection efficiency and spin polarization efficiency.

    STTR Phase II 2005 Department of DefenseAir Force
  2. Controllable Atomization for Supercritical Combustion

    SBC: Engi-Mat Co.            Topic: AF03T012

    nGimat Co., in collaboration with the Georgia Institute of Technology, and the Wright-Patterson AFB Air Force Research Laboratory, proposes to develop a fuel injection method and advanced numerical simulation tools for injection of fuel at supercritical conditions in aero-propulsion combustors. This project is designed to accelerate understanding and commercialization of transcritical and supercr ...

    STTR Phase II 2005 Department of DefenseAir Force
  3. Development of Bioassays for Prion Infectivity Using Human, Deer, or Elk Cells

    SBC: RURAL TECHNOLOGIES, INC.            Topic: A04T027

    The human infectivity of Chronic Wasting Disease (CWD) is unclear. Current diagnostics rely upon post-mortem examination and late-term disease. Migratory B cells are emerging as likely candidates for blood-borne infectivity, and therefore, a logical target for sensitive antemortem diagnosis. We have focused on the Follicular Dendritic Cell (FDC)-B cell interaction as a target to expand prions. Th ...

    STTR Phase II 2005 Department of DefenseArmy
  4. Combustion-Based Actuator for Flow Control in Transonic Flight Applications

    SBC: Virtual Aerosurface Technologies, Inc.            Topic: AF03T014

    Combustion powered actuation (COMPACT) is a flow control technology developed at Georgia Tech which utilizes a miniature combustion chamber (cubic centimeter scale) to produce high-speed pulsed jets suitable for aerodynamic flow control (separation control, drag reduction, shock control, etc.) at transonic or supersonic speeds. The system is lightweight, can be operated with passive fluidic valve ...

    STTR Phase II 2005 Department of DefenseAir Force
US Flag An Official Website of the United States Government