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

  1. ENHANCED CHROMOPHORE POLYMERIC NLO MATERIALS

    SBC: ADTECH SYSTEMS RESEARCH INC            Topic: N/A

    NONLINEAR OPTICAL MATERIALS ARE REQUIRED FOR A VARIETY OF POTENTIAL AIR FORCE APPLICATIONS INCLUDING OPTICAL SIGNAL PROCESSING (SWITCHES, MODULATORS, AND GUIDED WAVE DEVICES), AND NEW LASER SOURCES (OPTICAL PARAMETRIC OSCILLATORS AND HARMONIC GENERATORS). HOWEVER, PRESENTLY AVAILABLE MATERIALS ARE UNSATISFACTORY FOR MANY APPLICATIONS DUE TO SMALL NONLINEARITIES, POOR OPTICAL CLARITY, LONG RESPONSE ...

    SBIR Phase II 1993 Department of DefenseAir Force
  2. A MODEL FOR PREDICTING MMC RESPONSE UNDER MULTIAXIAL LOADING

    SBC: ADTECH SYSTEMS RESEARCH INC            Topic: N/A

    N/A

    SBIR Phase I 1993 Department of DefenseAir Force
  3. Fracture Mechanics Based Life Prediction of High Temperature Composite Joints

    SBC: ADTECH SYSTEMS RESEARCH INC            Topic: N/A

    N/A

    SBIR Phase I 1993 Department of DefenseAir Force
  4. Automating the Creation of Technical Software

    SBC: American Computational Tech            Topic: N/A

    Simulation provides a means of duplicating the operating environment of a topic of interest in a laboratory setting, but the environment itself is rarely the topic of interest. Providing the simulated environment requires access to personnel with expertise in the environment but without expertise in the topic actually to be studied, consuming resources but only providing the means to complete the ...

    SBIR Phase I 1993 Department of DefenseAir Force
  5. NOVEL DIAMOND/C/C COMPOSITES FOR THERMAL MANAGEMENT

    SBC: Applied Sciences            Topic: N/A

    AN INNOVATIVE INTEGRAL DIELECTRIC HEAT SINK MATERIAL, DIAMOND/CARBON/CARBON COMPOSITE, IS PROPOSED IN THIS PHASE I RESEARCH FOR THE USE IN FUTURE ADVANCED ELECTRONIC DEVICES. CARBONE/CARBONE COMPOSITE HAS A HIGHER THERMAL CONDUCTIVITY AND LOWER DENSITY, AND THEREFORE A HIGHER SPECIFIC THERMAL CONDUCTIVITY, AS COMPARED TO METALS. HOWEVER, CARBON IS ALSO AN ELECTRIC CONDUCTOR. WE PROPOSE TO APPLY DI ...

    SBIR Phase II 1993 Department of DefenseAir Force
  6. VIRTUAL PROTOTYPING TOOLS FOR SEMICONDUCTOR FABRICATION EQUIPMENT

    SBC: CFD Research Corporation            Topic: N/A

    THE EXISTING METHODOLOGY OF DESIGN AND FABRICATION OF SEMICONDUCTOR MANUFACTURING EQUIPMENT IS AN EXPENSIVE AND TIME CONSUMING PROCESS. TO KEEP PACE WITH THE RAPIDLY ADVANCING SEMICONDUCTOR INDUSTRY, IT IS NECESSARY TO DEVELOP A COMPUTER BASED ENVIRONMENT TO QUICKLY SIMULATE THE FEATURES OF THE MANUFACTURING EQUIPMENT BEFORE IT IS TURNED INTO A PHYSICAL PROTOTYPE. APART FROM ACHIEVING CONSIDERABLE ...

    SBIR Phase II 1993 Department of DefenseDefense Advanced Research Projects Agency
  7. INFLUENCE OF SUPERCRITICAL CONDITIONS ON PRECOMBUSTION CHEMISTRY AND TRANSPORT BEHAVIOR OF JET FUELS

    SBC: CFD Research Corporation            Topic: N/A

    ADVANCED ENGINE TECHNOLOGY AND HYPERSONIC FLIGHT SPEEDS OF FUTURE MILITARY AIRCRAFTS PLACE INCREASING HEAT LOAD ON JET FUELS. THE INCREASE IN HEAT LOAD PUSH THE OPERATION OF FUELS INTO THEIR SUPERCRITICAL REGIME. THE PERFORMANCE OF FUTURE AIRCRAFT WILL BE SERIOUSLY LIMITED IF FUELS CANNOT BE OPERATED EFFECTIVELY AT SUPERCRITICAL CONDITIONS. THE PRECOMBUSTION CHEMISTRY AND TRANSPORT PROCESSES AT TH ...

    SBIR Phase II 1993 Department of DefenseAir Force
  8. RAMBURNER FUEL INJECTOR FOR ENDOTHERMIC FUELS

    SBC: CFD Research Corporation            Topic: N/A

    For sustained high speed flight (Mach 3-6), recent studies have shown that endothermic fuels are required to cool aircraft systems. Such a cooling system would deliver fuel to the ramburner in varying amounts of liquid and gaseous phases. This project proposes to experimentally investigate and develop an innovative dual-phase fuel injector prototype suitable for crossflow injection in ramburners. ...

    SBIR Phase I 1993 Department of DefenseAir Force
  9. AN INNOVATIVE AIR-TURBO ROCKER (ATR) SCRAMJET PROPULSION SYS AND SUPPORTING DESIGN APPROACH

    SBC: CFD Research Corporation            Topic: N/A

    N/A

    SBIR Phase I 1993 Department of DefenseAir Force
  10. ULTRA LOW COST ENGINE CONTROL SYSTEM

    SBC: Electronic Concepts &            Topic: N/A

    PRESENT TURBOJET ENGINE CONTROL SYSTEMS, WHICH ARE COMPRISED OF: CONTROLLER, FUEL METERING DEVICE, SENSORS, CONNECTORS, AND HARNESSES ARE THE SINGLE MOST EXPENSIVE SUBSYSTEM ON EXPENDABLE TURBOJET ENGINES. THE SIZE AND COST OF EXPENDABLE TURBOJET ENGINES HAS STEADILY DECREASED. HOWEVER, THE ENGINE CONTROL SYSTEM COST HAS RE MAINED RELATIVELY CONSTANT. ELECTRONIC CONCEPTS PROPOSES TO DEMONSTRATE TH ...

    SBIR Phase II 1993 Department of DefenseDefense Advanced Research Projects Agency

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