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. 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
  2. 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
  3. 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
  4. 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 ForceDepartment of DefenseDepartment of Defense
  5. 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 ForceDepartment of DefenseDepartment of Defense
  6. 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
  7. 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
  8. Plasma Induced Micro Flame Ionization Detector for Environmental Monitoring

    Amount: $99,478.00

    Abstract

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

    Amount: $99,974.00

    Advances in high power, photovoltaic technology has enabled the possibility of reasonably sized, high specific power, high power, solar arrays. New thin film solar arrays have demonstrated specific p ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  10. Fiber-Coupled Spectrometer for TPS Materials

    Amount: $99,983.00

    Heat shield technology is a critical component of manned spaceflight. In particular, the new Crew Exploration Vehicle (CEV) requires thermal protection systems (TPS) beyond the current state of the a ...

    SBIR Phase I 2010 National Aeronautics and Space Administration

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