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A review of Hall thruster plume modeling [PDF]

open access: yes38th Aerospace Sciences Meeting and Exhibit, 2000
Hall thrusters are an attractive form of electric propulsion that are being developed to replace chemical systems for many orbit propulsion tasks on communications satellites. A concern in the use of these devices is the possible damage their plumes may cause to the host spacecraft.
AIAA   +14 more
openaire   +4 more sources

Application of electric thrusters in a spacecraft propulsion system [PDF]

open access: yesКосмические аппараты и технологии, 2022
The place of electric rocket thrusters in a spacecraft propulsion system is pointed out; the tasks for such propulsion system are described. The modern classification of electric thrusters is given, in accordance of that one there are four classes ...
N. E. Kovalenko, A. A. Vnukov
doaj   +1 more source

Comparative analysis of simulation and experiment for the Hall-type thruster BPT-4000

open access: yesResults in Engineering, 2023
Since 2004, the Plasma Physics Laboratory (PPL/PI/UnB) has been developing permanent magnet Hall thrusters due to their high efficiency. However, permanent magnets have limited use due to their maximum working temperature (the point at which they begin ...
Marconi C. Porto   +3 more
doaj   +1 more source

2D Fluid-PIC Simulations of Hall Thrusters with Self-Consistent Resolution of the Space-Charge Regions

open access: yesPlasma, 2023
Many hybrid simulations of Hall thrusters, where electrons and ions are solved using hydrodynamics and particle-in-cell methods, respectively, assume that the ionized gas is quasi-neutral everywhere in the computational domain and apply so-called thin ...
Alejandro Lopez Ortega   +1 more
doaj   +1 more source

In situ erosion measurement tools for electric propulsion thrusters: triangular laser head and telemicroscope

open access: yesEPJ Techniques and Instrumentation, 2022
The lifetime of electric propulsion (EP) thrusters depends particularly on the erosion characteristics of operation relevant components, for instance, the grid hole erosion of gridded ion thrusters or the channel wall erosion of Hall effect thrusters ...
Carsten Bundesmann   +8 more
doaj   +1 more source

Small Hall Effect Thruster with 3D Printed Discharge Channel: Design and Thrust Measurements

open access: yesAerospace, 2021
This paper presents the design and performance of the UAH-78AM, a low-power small Hall effect thruster. The goal of this work is to assess the feasibility of using low-cost 3D printing to create functioning Hall thrusters, and study how 3D printing can ...
Ethan P. Hopping   +2 more
doaj   +1 more source

NASA's Hall thruster program [PDF]

open access: yes37th Joint Propulsion Conference and Exhibit, 2001
NASA's Hall thruster program has base research and focused development efforts in support of the Advanced Space Transportation Program, Space-Based Program, and various other programs. The objective of the base research is to gain an improved understanding of the physical processes and engineering constraints of Hall thrusters to enable development of ...
Robert Jnkovsky   +7 more
openaire   +2 more sources

An integrated fluid simulation platform on Hall thruster plasmas

open access: yesAIP Advances, 2022
In this work, a newly integrated fluid simulation platform, named DUT-HTFS, is developed for the multiple physical fields in Hall thrusters. The integrated simulation platform includes three inter-related parts: the geometry module, background magnetic ...
Nannan Li   +3 more
doaj   +1 more source

Axisymmetric Hybrid Plasma Model for Hall Effect Thrusters

open access: yesParticles, 2021
Hall Effect Thrusters (HETs) are nowadays widely used for satellite applications because of their efficiency and robustness compared to other electric propulsion devices.
Mario Panelli   +4 more
doaj   +1 more source

On the onset of breathing mode in Hall thrusters and the role of electron mobility fluctuations

open access: yesFrontiers in Physics, 2022
Breathing mode is an ionization instability which is observed ubiquitously in the operation of Hall thrusters. It is recognized as a relatively low frequency (10–30 kHz) longitudinal oscillation of the discharge current and the plasma parameters ...
L. Leporini    +7 more
doaj   +1 more source

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