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UID:0-483@aerospace.technion.ac.il

DTSTART;TZID=Asia/Jerusalem:20160411T163000

DTEND;TZID=Asia/Jerusalem:20160411T173000

DTSTAMP:20230603T191644Z

URL:https://aerospace.technion.ac.il/events/numerical-and-experimental-inv
 estigations-of-the-camila-hall-thruster-plume/

SUMMARY:Numerical and Experimental Investigations of the CAMILA Hall Thrust
 er Plume
DESCRIPTION:Lecturer:Matteo Laterza\n Faculty:Department of Aerospace Engin
 eering\n Institute:Technion – Israel Institute of Technology\n Location:
 Classroom 165\, ground floor\, Library\, Aerospace Eng.\n Zoom: \n Abstrac
 t: \n Details: \n This work focuses on the characterization of the plume o
 f the CAMILA Hall thruster. A numerical model is developed and implemented
  in a computational code using a hybrid Particle-In-Cell scheme. A series 
 of Langmuir probe measurements is performed in the plume at 1m downstream 
 of the thruster. These measurements are used along with existing data to v
 alidate the numerical model.\nThe developed code is then used to analyze p
 lume behavior at different operating points. A two thruster cluster is als
 o simulated in different configurations to test plume interactions in conv
 erging clusters and to determine optimal convergence angles for thrust vec
 toring. It was found that the plume interactions manage to decrease plume 
 divergence\, contrary to what expected. An optimal vectoring configuration
  was also found for deflection angles up to 10°.
CATEGORIES:Seminars
LOCATION:Classroom 165\, ground floor\, Library\, Aerospace Eng.

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DTSTART:20160325T030000

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