M-DOT Aerospace

Address

3418 South 48th Street, Suite 3
Phoenix, AZ, -

http://www.m-dot.com

Information

DUNS: 612149138
# of Employees: 28

Ownership Information

Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N

Award Charts




Award Listing

  1. Low-Cost Ball/Air/Magnetic Hybrid Bearing System for Extended-Life Micro Gas Turbine Engines

    Amount: $69,996.00

    The Team of M-DOT Aerospace and University of Texas, Arlington propose to analyze, construct and test a 40 mm foil thrust bearing featuring a unique bump foil concept and top-foil profile designed by ...

    STTRPhase I2010Navy Department of Defense
  2. Microsupercharger and/or Turbocharger for Small, Heavy Fuel Engines

    Amount: $749,774.00

    M-DOT proposes to team with engine developers and produce a turbocharger for an HFE that will support a range of power levels from 30 to 60 HP. The launch design application will be a heavy fuel conv ...

    SBIRPhase II2010Department of Defense Air Force
  3. Very High Altitude Aircraft Propulsion Engines

    Amount: $748,565.00

    M-DOT Aerospace proposes to team with Mezzo Technologies of Baton Rouge LA and Dr. Hui Wang of the USC, LA and conduct a series of tests and analyses that address all currently perceived critical-path ...

    SBIRPhase II2009Defense Advanced Research Projects Agency Department of Defense
  4. Microsupercharger and/or Turbocharger for Small, Heavy Fuel Engines

    Amount: $99,996.00

    Proposed is the preliminary design of an extremely small turbocharger sized for an 8 to 12 hp class engine. The entire unit will weigh roughly 240 grams. Design will incorporate pre-existing compress ...

    SBIRPhase I2008Department of Defense Air Force
  5. Portable Cogeneration of Power and Cooling

    Amount: $99,998.00

    Proposed is a combined electric power and cooling system that shares a common proprietary working fluid. Employing this fluid enables practical application of both systems in a combined unit. The en ...

    SBIRPhase I2007Department of Defense Navy
  6. Improved Bearing Compartment Sealing for Gas Turbine Engines

    Amount: $99,982.00

    A technical approach to gas path seal design is described that provides a unique combination of benefits. It has broad application to gas seals including those applied to bearing sumps and gas paths. ...

    SBIRPhase I2007Air Force Department of Defense
  7. Very High Altitude Aircraft Propulsion Engines

    Amount: $198,542.00

    Proposed is a power system suitable for operation to altitudes of 100K feet or more and capable of operating for 12-20 hours at a time. The system will be storable for years in a sealed container. I ...

    SBIRPhase I2007Defense Advanced Research Projects Agency Department of Defense
  8. Novel Propulsion Using Humphrey Cycle or Other Concepts

    Amount: $98,927.00

    M-DOT proposes to study application of a proprietary rotary expander as a quasi-Constant-Volume Combustor (CVC) in a gas turbine. Whereas CVC has been explored as a topping element (to increase max c ...

    SBIRPhase I2005Defense Advanced Research Projects Agency Department of Defense
  9. Small, Low Cost, High Perforamnce Engine for Miniature Munitions

    Amount: $749,890.00

    Based on the positive results obtained from the cycle analysis and preliminary design conducted during Phase I, M-DOT Aerospace proposes to design, analyze, fabricate and test a low-cost high-bypass t ...

    SBIRPhase II2003Air Force Department of Defense
  10. Small, Low Cost, High Performance Engines for Miniature Munitions

    Amount: $99,807.00

    "We propose to design and develop a turbine-driven fan module that will attach to the exhaust duct of an expendable turbojet converting it into an aft-fan turbofan. Depending upon selected bypass rat ...

    SBIRPhase I2002Air Force Department of Defense

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