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 the channel walls in a Hall plasma accelerator

IG Mikellides, I Katz, RR Hofer, DM Goebel… - Physics of …, 2011 - pubs.aip.org
In a qualification life test of a Hall thruster it was found that the erosion of the acceleration
channel practically stopped after∼ 5600 h⁠. Numerical simulations using a two …

Survey of moderate-power electric propulsion systems

EM Petro, RJ Sedwick - Journal of Spacecraft and Rockets, 2017 - arc.aiaa.org
ELECTRIC propulsion (EP) systems have become an integral component of space mission
architectures. The field of EP has grown to include unique systems that fill niches from …

Demonstration of 10,400 hours of operation on 4.5 kw qualification model hall thruster

K de Grys, A Mathers, B Welander… - 46th AIAA/ASME/SAE …, 2010 - arc.aiaa.org
Between 2007 and 2009, Aerojet and Lockheed Martin Space Systems Company (LMSSC)
successfully extended the demonstrated operating duration of the qualification model BPT …

Magnetic shielding of the acceleration channel walls in a long-life Hall thruster

I Mikellides, I Katz, R Hofer, D Goebel… - 46th AIAA/ASME/SAE …, 2010 - arc.aiaa.org
I. Introduction all thrusters provide an attractive combination of thrust and specific impulse for
a variety of near-earth missions. In many cases these systems allow for significant …

Efficacy of electron mobility models in hybrid-PIC Hall thruster simulations

R Hofer, I Katz, D Goebel, K Jameson… - 44th AIAA/ASME/SAE …, 2008 - arc.aiaa.org
OMMERCIAL electric propulsion systems are now being considered as a cost effective
solution for competitively awarded science missions such as the NASA Discovery and New …

[HTML][HTML] An oxygen-fuelled Hall Effect Thruster: Channel length, ceramic walls and anode material experimental analyses

JM Tejeda, A Knoll - Acta Astronautica, 2023 - Elsevier
Abstract An oxygen-fuelled Hall Effect Thruster is investigated at the Imperial Plasma
Propulsion Laboratory vacuum chamber facilities over a different range of discharge …

Performance evaluation of the T6 ion engine

J Snyder, DM Goebel, RR Hofer, JE Polk… - Journal of Propulsion …, 2012 - arc.aiaa.org
WITH the recent launch of the Dawn spacecraft and the successful operation of its NSTAR
ion propulsion system [1], new and challenging deep space missions that can use ion …

Hall thruster cathode flow impact on coupling voltage and cathode life

DM Goebel, KK Jameson, RR Hofer - Journal of Propulsion and Power, 2012 - arc.aiaa.org
INTEREST in Hall thruster research and development has increased significantly in the
United States over the past 20 years. Hall thrusters offer several system advantages over ion …

Effects of internally mounted cathodes on Hall thruster plume properties

RR Hofer, LK Johnson, DM Goebel… - IEEE Transactions on …, 2008 - ieeexplore.ieee.org
The effects of cathode position on the operation and plume properties of an 8-kW Hall
thruster are discussed. Thruster operation was investigated at operating conditions ranging …