Directed Vapor Technologies International, Inc.

Company Information
Address 2 Boars Head Ln
Charlottesville, VA, 22903-4605

http://www.directedvapor.com

Information

DUNS: 036500804

# of Employees: 14


Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N



Award Charts




Award Listing

  1. Development of Marinized Protective Coatings for Higher Temperature Operations of Marine Gas Turbine Engines

    Amount: $749,994.00

    The marine environment is extremely corrosive to turbine engine components due to salt exposures from the sea, the presence of fuel impurities and the high temperatures experienced. To cope with futur ...

    SBIRPhase II2017Department of Defense Navy
  2. Scalable Manufacturing of Functional Yarns for Textile-based Energy Storage

    Amount: $149,772.00

    Smart textile technologies with advanced functionalities (e.g., sensing, physical actuation) are being developed for military and civilian applications. These products have, to date, been powered by c ...

    STTRPhase I2017Department of Defense Army
  3. Advanced Bond Coats for Thermal Barrier Coating Systems Based on High Entropy Alloys

    Amount: $998,533.00

    Compact Membrane Systems membranes have shown very stable performance. Operating for over 270 days with propylene/propane showed propylene flux of 175 GPU and propylene/propane selectivity of 30. Even ...

    SBIRPhase II2016Department of Energy
  4. Thermal Barrier Coatings for Long Life in Marine Gas Turbine Engines

    Amount: $79,925.00

    The marine environment is extremely corrosive to turbine engine components due to the large amount of salts from the sea coupled with the fuel impurities and the high temperatures experienced. To cope ...

    STTRPhase I2016Department of Defense Navy
  5. Advanced Bond Coats for Thermal Barrier Coating Systems Based on High Entropy Alloys

    Amount: $149,935.25

    Statement of the problem or situation that is being addressed. The availability of ultraclean (near-zero emission), abundant, low-cost domestic energy is critical to providing economic prosperity, str ...

    SBIRPhase I2015Department of Energy
  6. Robust High Temperature Environmental Barrier Coating System for Ceramic Matrix Composite Gas Turbine Components using Affordable Processing Approach

    Amount: $901,160.00

    Research is proposed to demonstrate the use of advanced manufacturing techniques to enable the affordable application of multi-functional thermal/environmental barrier coatings (T/EBCs) having enhance ...

    SBIRPhase II2015National Aeronautics and Space Administration
  7. High-Performance Magnesium Alloys and Composites by Efficient Vapor Phase Processing

    Amount: $999,804.00

    The low density of magnesium makes it of interest for the development of advanced materials having high specific strength and stiffness. Current Mg applications, however, are limited by the performanc ...

    STTRPhase II2015Department of Defense Army
  8. Development of Marinized Protective Coatings for Higher Temperature Operations of Marine Gas Turbine Engines

    Amount: $79,891.00

    The marine environment is extremely corrosive to turbine engine components due to salt exposures from the sea, the presence of fuel impurities and the high temperatures experienced. To cope with futur ...

    SBIRPhase I2015Department of Defense Navy
  9. Robust High Temperature Environmental Barrier Coating System for Ceramic Matrix Composite Gas Turbine Components using Affordable Processing Approach

    Amount: $121,972.00

    Research is proposed to demonstrate the use of advanced manufacturing techniques to enable the affordable application of multi-functional thermal / environmental barrier coatings (T/EBCs) having enhan ...

    SBIRPhase I2014National Aeronautics and Space Administration
  10. Advanced Deposition Capability for Oxidation & Corrosion Protection Coatings

    Amount: $868,601.00

    NASA's long range goals of reducing fuel consumption by 30% and increasing fuel efficiency by 35% can be partially accomplished through increasing the operation temperatures of gas turbine engines. T ...

    STTRPhase II2014National Aeronautics and Space Administration

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