ELECTRODYNAMIC APPLICATIONS INC

Basic Information

3600 GREEN CT STE 300
ANN ARBOR, MI, 48105-1570

http://www.edapplications.com/

Company Profile

n/a

Additional Details

Field Value
DUNS: 610511334
Hubzone Owned: N
Socially and Economically Disadvantaged: Y
Woman Owned: N
Number of Employees: 8


  1. Integrated Energetic Ion Mitigation for High Power Plasma Cathodes

    Amount: $124,978.00

    The innovation proposed is a hollow cathode that integrates mitigation methods to suppress wear to the keeper. Recent advances in the magnetic topology in Hall thrusters has eliminated erosion of th ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  2. Divergent Field Annular Ion Engine

    Amount: $124,793.00

    The proposed work investigates an approach that would allow an annular ion engine geometry to achieve ion beam currents approaching the Child-Langmuir limit. In this respect, the annular engine, whos ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  3. Fiber-Optic Pyrometer for Thermal Protection Systems

    Amount: $124,935.00

    Surface temperatures in atmospheric reentry simulations range from 1500-2300 K, while stagnation temperature on the leading edge of a Mach 6 flight vehicle at 25 km altitude is 1817 K. Sensors that c ...

    SBIR Phase I 2013 National Aeronautics and Space Administration
  4. Energetic Ion Mitigation Methodology for High Power Plasma Thruster Cathodes

    Amount: $199,725.00

    The presence of energetic ions, that appear under high cathode current operation, stand as a showstopper to the realization of high power electric propulsion. Physical barriers such as the use of ca ...

    SBIR Phase I 2013 National Aeronautics and Space Administration
  5. Nonintrusive fiber interferometer for ablative TPS recession measurement

    Amount: $99,997.00

    ABSTRACT: The next generation of hypersonic and reentry vehicles being designed for the Department of Defense (DoD) applications will require advanced Thermal Protection System (TPS). While new TPS ...

    STTR Phase I 2012 Air Force Department of Defense
  6. Hybrid Chemical-Electric Propulsion (HCEP)

    Amount: $99,649.00

    ABSTRACT: The proposed Phase I efforts seek to develop a dual-mode Hybrid ChemicalElectric Propulsion thruster concept design based on the extensive microwave torch/arcjet experience of PSU and Hall ...

    STTR Phase I 2012 Air Force Department of Defense
  7. Fiber-Coupled Spectrometer for TPS Materials

    Amount: $599,972.00

    EDA, Inc., in partnership with Penn State, has shown previously that the concept of embedding fiber optics within ablative TPS material has merit and should yield a successful implementation of a spec ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  8. High Power High Thrust Ion Thruster (HPHTion): 50 CM Ion Thruster for Near-Earth Applications

    Amount: $599,242.00

    Advances in high power, photovoltaic technology has enabled the possibility of reasonably sized, high specific power, high power, solar arrays. At high specific powers, power levels ranging from 50 t ...

    STTR Phase II 2011 National Aeronautics and Space Administration
  9. Plasma Induced Micro Flame Ionization Detector for Environmental Monitoring

    Amount: $99,478.00

    Abstract

    SBIR Phase I 2011 National Aeronautics and Space Administration
  10. Optimized Drying of Nano sized anisotropic particles in suspensions to improved aerosol dispersions.

    Amount: $99,858.00

    The US Army has underscored the importance of developing more effective obscurant material for shielding US soldiers and their equipment from visible, microwave, and infrared observation. Current sep ...

    STTR Phase I 2010 Army Department of Defense

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