Time-resolved ion velocity distribution in a cylindrical Hall thruster: heterodyne-based experiment and modeling.

نویسندگان

  • A Diallo
  • S Keller
  • Y Shi
  • Y Raitses
  • S Mazouffre
چکیده

Time-resolved variations of the ion velocity distribution function (IVDF) are measured in the cylindrical Hall thruster using a novel heterodyne method based on the laser-induced fluorescence technique. This method consists in inducing modulations of the discharge plasma at frequencies that enable the coupling to the breathing mode. Using a harmonic decomposition of the IVDF, one can extract each harmonic component of the IVDF from which the time-resolved IVDF is reconstructed. In addition, simulations have been performed assuming a sloshing of the IVDF during the modulation that show agreement between the simulated and measured first order perturbation of the IVDF.

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Time-Dependent Ion Velocity Distribution: A novel Heterodyne Laser-Induced Fluorescence with Coupled Wave Excitation

We propose a laser induced fluorescence heterodyne approach to resolve the timedependent ion velocity distribution (IVDF) in a Hall thruster. This approach is motivated by studies of low frequency modes of oscillations in Hall thruster, including azimuthal or so-called spoke and axial or so-called breathing oscillations. In this paper, we present the first successful application of this method ...

متن کامل

Preliminary Measurements of Time-Resolved Ion Velocity Distributions Near a Hollow Cathode

Presented are preliminary measurements of near-cathode ion velocity distributions using time-resolved laser induced fluorescence. Two experiments were performed. First, time-averaged velocity distributions were measured in a LaB6 hollow cathode plume under the influence of a Hall thruster magnetic field provided by the 6-kW H6 thruster. The discharge was sustained without a downstream anode but...

متن کامل

Modeling a Hall Thruster from Anode to Plume Far Field

MODELING A HALL THRUSTER FROM ANODE TO PLUME FAR FIELD AFOSR GRANT FA9550-05-l-0042 lain D. Boyd Department of Aerospace Engineering University of Michigan Ann Arbor, MI 48109-2140 Hall thrusters represent an efficient form of electric propulsion that is being implemented on USAF satellites for station-keeping tasks. Numerical simulation of the plasma flow inside Hall thrusters is playing an in...

متن کامل

Time-evolution of the ion velocity distribution function in the discharge of a Hall effect thruster

The temporal characteristics of the Xe ion axial Velocity Distribution Function (VDF) were recorded in the course of low-frequency discharge current oscillations (∼ 14kHz) of the 5 kW-class PPSrX000 Hall thruster. The evolution in time of the ion axial velocity component is monitored by means of a laser induced fluorescence diagnostic tool with a time resolution of 100ns. As the number of fluor...

متن کامل

Ion Velocity and Plasma Potential Measurements of a Cylindrical Cusped Field Thruster

Measurements of the most probable time-averaged axial ion velocities and plasma potential within the acceleration channel and in the plume of a straightchanneled cylindrical cusped field thruster operating on xenon are presented. Ion velocities for the thruster are derived from laser-induced fluorescence measurements of the 5d[4]7/2 −6p[3]5/2 xenon ion excited state transition centered at λ = 8...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

عنوان ژورنال:
  • The Review of scientific instruments

دوره 86 3  شماره 

صفحات  -

تاریخ انتشار 2015