Daedalus Research Inc.

Basic Information

P.O. Box 6067
Logan, UT, 84341

Company Profile

n/a

Additional Details

Field Value
DUNS: n/a
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 8


  1. Ion Propulsion for MEMS Flight Vehicles (rev 7-1)

    Amount: $97,426.00

    A novel approach to the propulsion of very small, micro air vehicles is proposed in which electrostatic forces acting between an ion gas cloud and an appropriate anode are harnessed for thrust or lift ...

    SBIR Phase I 1996 Defense Advanced Research Projects Agency Department of Defense
  2. FEASIBILITY OF UAV AIRFOIL & CONTROL SURFACE MANUFACTURING USING CONTINUOUS MANUFACTURING MACHINES

    Amount: $277,477.00

    CONTRACTOR WILL EXAMINE THE FEASIBILITY OF UTILIZING PULTRUSION-TYPE CONTINUOUS TAPE LAYING MANUFACTURING EQUIPMENT TO FABRICATE COMPOSITE SANDWICH STRUCTURE WINGS AND STABILIZERS FOR CLOSE RANGE AND ...

    SBIR Phase II 1993 Defense Advanced Research Projects Agency Department of Defense
  3. VTOL PROPULSION BOOST BY MEANS OF TORQUE AUGMENTATION FROM AN ELECTRIC MACHINE.

    Amount: $53,628.00

    CONTRACTOR WILL EXAMINE THE FEASIBILITY OF HYBRID POWERPLANTS IN SMALL V/STOL AIR VEHICLES THAT COMBINE INTERNAL COWBUSTION (IC) ENGINESAND PULSED POWER ELECTRICAL AUGMENTATION MACHINES. THE IC ENGINE ...

    SBIR Phase I 1991 Navy Department of Defense
  4. FEASIBILITY OF UAV AIRFOIL & CONTROL SURFACE MANUFACTURING USING CONTINUOUS MANUFACTURING MACHINES

    Amount: $54,239.00

    N/A

    SBIR Phase I 1991 Defense Advanced Research Projects Agency Department of Defense
  5. FEASIBILITY OF ROUGH TERRAIN/WILD WEATHER BASING OF SLAVED TANDEM FREEWING (STF) UAVS

    Amount: $416,059.00

    A SLAVED TANDEM FREEWING (STF) AIRCRAFT IS A NOVEL, TANDEM WING, V/STOL AIR VEHICLE CONFIGURATION WITH UNIQUE POTENTIAL FOR SELFLAUNCHING AND SELF-RECOVERY FROM BASES WITHOUT FLAT AND EVEN PLATFORMS ( ...

    SBIR Phase II 1990 Defense Advanced Research Projects Agency Department of Defense
  6. FEASIBILITY OF PROPELLER LOAD CONTROL STRATEGIES UTILIZING PIEZOCERAMIC DRIVERS

    Amount: $52,477.00

    CONTRACTOR WILL EXAMINE THE FEASIBILITY OF UTILIZING ITS PIEZOCERAMIC CHIPS AS ACTUATORS FOR VARIABLE TWIST PROPELLERS IN UAV APPLICATIONS. THESE ACTUATORS WILL BE UTILIZED TO OPTIMIZE THE TWIST OF RI ...

    SBIR Phase I 1990 Navy Department of Defense
  7. FEASIBILITY OF VARIOUS EROSION RESISTANCE/EROSION AVOIDANCE TECHNIQUES FOR SMALL INEXPENSIVE PROPELLERS

    Amount: $53,511.00

    CONTRACTOR WILL EXAMINE THE FEASIBILITY OF UTILIZING ITS EXISTING, BUT EXPERIMENTAL LEADING-EDGE PROTECTION SYSTEM TO PROVIDE EROSION RESISTANCE FOR INEXPENSIVE UAV PROPELLERS. THE EXISTING SYSTEM UTI ...

    SBIR Phase I 1990 Navy Department of Defense
  8. FEASIBILITY OF ROUGH TERRAIN/WILD WEATHER BASING OF SLAVED TANDEM FREEWING (STF) UAVS

    Amount: $53,961.00

    N/A

    SBIR Phase I 1989 Defense Advanced Research Projects Agency Department of Defense
  9. ELIMINATION OF TURBULENCE-INDUCED STRUCTURAL FAILURE AND CONTROL LOSS IN VERY LIGHT AIRCRAFT

    Amount: $300,000.00

    A SYSTEM UTILIZING THE FREE-WING CONCEPT HAS BEEN DESIGNED FOR LIGHT AND VERY LIGHT WING-LOADING AIRCRAFT THAT ACCOMMODATES MODERATE TO HEAVY TURBULENCE WITHOUT TRANSMITTING HIGH GUST LOADINGS TO THE ...

    SBIR Phase II 1985 Department of Transportation
  10. ELIMINATION OF TURBULENCE-INDUCED STRUCTURAL FAILURE AND CONTROL LOSS IN VERY LIGHT AIRCRAFT

    Amount: $49,909.00

    N/A

    SBIR Phase I 1984 Department of Transportation

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