Miniaturization perspectives of electrostatic propulsion for small spacecraft platforms

SH Yeo, H Ogawa, D Kahnfeld, R Schneider - Progress in Aerospace …, 2021 - Elsevier
In-space electric propulsion technologies have advanced significantly in the last decade,
while there has been increasing interest in economical propulsion systems with growing …

Magnetic shielding of a laboratory Hall thruster. I. Theory and validation

IG Mikellides, I Katz, RR Hofer… - Journal of Applied Physics, 2014 - pubs.aip.org
We demonstrate a technique by which erosion of the acceleration channel in Hall thrusters
can be reduced by at least a few orders of magnitude. The first principles of the technique …

Recommended practice for use of Faraday probes in electric propulsion testing

DL Brown, MLR Walker, J Szabo, W Huang… - Journal of Propulsion …, 2017 - arc.aiaa.org
Faraday probes are a common plasma diagnostic used to determine the local ion charge
flux of electric propulsion plumes. Standard practices, guidelines, and recommendations are …

Review on the properties of hexagonal boron nitride matrix composite ceramics

X Duan, Z Yang, L Chen, Z Tian, D Cai, Y Wang… - Journal of the European …, 2016 - Elsevier
Novel hexagonal boron nitride (h-BN) matrix composite ceramics exhibit versatile and
greatly improved properties compared with the traditional h-BN ceramics, such as excellent …

Numerical modeling of high efficiency multistage plasma thrusters for space applications

D Kahnfeld, J Duras, P Matthias, S Kemnitz… - Reviews of Modern …, 2019 - Springer
The high efficiency multistage plasma-thruster (HEMP-T) represents an ion thruster
technology that was developed by Thales Deutschland GmbH beginning in the early 2000s …

Foundations of plasmas as ion sources

B Jorns, T Lafleur - Plasma Sources Science and Technology, 2023 - iopscience.iop.org
An overview of low temperature, partially magnetized ion sources is presented. This class of
devices is broadly characterized by plasma densities below 10 19 m− 3, electron …

Facility pressure effects on a Hall thruster with an external cathode: I. Numerical simulations

AL Ortega, IG Mikellides, VH Chaplin… - Plasma Sources …, 2020 - iopscience.iop.org
We employ the 2D (r–z) code Hall2De to conduct numerical simulations of the SPT-140, a
Hall thruster that operates with an external hollow cathode. The simulations are informed by …

Design of a laboratory Hall thruster with magnetically shielded channel walls, phase III: Comparison of theory with experiment

I Mikellides, I Katz, R Hofer, D Goebel - 48th AIAA/ASME/SAE/ASEE …, 2012 - arc.aiaa.org
A proof-of-principle effort to demonstrate a technique by which erosion of the acceleration
channel in Hall thrusters can be eliminated has been completed successfully. The first …

Carbon Back Sputter Modeling for Hall Thruster Testing

JH Gilland, G Williams, JM Burt, J Yim - 52nd AIAA/SAE/ASEE Joint …, 2016 - arc.aiaa.org
I. Introduction o demonstrate high-power, high-specific-impulse performance for the Asteroid
Redirect Robotic Mission (ARRM), both in terms of desired mission capability and required …

Plasma-induced erosion on ceramic wall structures in Hall-effect thrusters

T Burton, AM Schinder, G Capuano, JJ Rimoli… - Journal of Propulsion …, 2014 - arc.aiaa.org
A 60 wt% boron nitride (BN)–40 wt% silica (SiO 2) hot-pressed composite, denoted as M26,
was used as the insulating chamber wall for a xenon plasma Hall-effect thruster operated for …