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  1. iopscience.iop.org

    Sep 20, 2024In this work a complete atmospheric EHD thruster is tested in a subsonic wind tunnel,
with the purpose of evaluating changes in performance due to simulated flight conditions
and, for the first time, comparing them with a physical model of the drift region.
  2. Was this helpful?
  3. researchgate.net

    Sep 20, 2024In this work a complete atmospheric EHD thruster is tested in a subsonic wind tunnel, with the purpose of evaluating changes in performance due to simulated flight conditions and, for the first ...
  4. Was this helpful?
  5. Sep 2, 2024Repository relative to article "Wind Tunnel Testing and Performance Modeling of an Atmospheric Ion Thruster" ... Skip to main. Communities. My dashboard. Log in Sign up IPROP Community. Published 2024 ... Repository relative to article "Wind Tunnel Testing and Performance Modeling of an Atmospheric Ion Thruster" Files. readme.txt. Files ...
  6. iprop-project.eu

    The test campaign also revealed that the maximum operating voltage increases with respect to still air conditions, leading to a further chance of creating a larger thrust. A recent DOI n. 10.1088/1361-6463/ad7d9c has been assigned to the article "Wind Tunnel Testing and Performance Modeling of an Atmospheric Ion Thruster"
  7. iprop-project.eu

    This project aims to bring ionic air-breathing propulsive systems beyond the pioneering phase, exploring their capabilities and improving their performance. Non-thermal plasma for atmospheric propulsion is a subject of recent investigations: model airplanes and vertical lifters have recently flown with this type of propulsion, but the potential ...
  8. politesi.polimi.it

    Apr 9, 2024This thesis aims to investigate how the performance of the thruster changes when subjected to an external convective flow. To conduct the tests, it was necessary to redesign the thruster structure to allow its positioning in a wind tunnel. The module has a fixed configuration, with geometric parameters chosen based on optimization results ...
  9. ui.adsabs.harvard.edu

    In this work a complete atmospheric electro-hydro-dynamic (EHD) thruster is tested in a subsonic wind tunnel, with the purpose of evaluating changes in performance due to simulated flight conditions and, for the first time, comparing them with a physical model of the drift region. An aerodynamic frame was designed to accommodate the electrodes inside the wind tunnel.
  10. ntrs.nasa.gov

    The wind tunnel, test stand, 699 rotor, and auxiliary equipment are described in this section. This section updates and expands on material originally presented in Ref. 1. NFAC Wind Tunnel The TTR was designed specifically for operations in the NFAC, which is located at Ames Research

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