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 …

Electric micropropulsion systems

WP Wright, P Ferrer - Progress in Aerospace Sciences, 2015 - Elsevier
With the development of microspacecraft, the field of electrical micropropulsion is a rapidly
expanding discipline. New ideas are being explored constantly and a review of the current …

[HTML][HTML] Performance measurement and evaluation of an ionic liquid electrospray thruster

C Huang, LI Jianling, LI Mu - Chinese Journal of Aeronautics, 2023 - Elsevier
As a novel micro-propulsion system for small satellites (from micro to nano), the ionic liquid
electrospray propulsion system is a promising candidate. However, performance …

[HTML][HTML] Performance of a low power Hall effect thruster with several gaseous propellants

TF Munro-O'Brien, CN Ryan - Acta Astronautica, 2023 - Elsevier
There is a growing need to consider alternative propellants for operation in Hall thrusters,
away from the conventional legacy of using xenon. This is particularly the case for small Hall …

Performance characterization of a low-power magnetically shielded Hall thruster with an internally-mounted hollow cathode

RW Conversano, RB Lobbia, TV Kerber… - Plasma Sources …, 2019 - iopscience.iop.org
Magnetically shielded miniature (MaSMi) is a low power (≤ 1 kW) long life (> 100 kg Xe
throughput) magnetically shielded Hall thruster that features an internally mounted hollow …

Finite pressure effects in magnetically shielded Hall thrusters

RR Hofer, JR Anderson - 50th AIAA/ASME/SAE/ASEE Joint Propulsion …, 2014 - arc.aiaa.org
We describe the effects of finite pressure in a large vacuum facility on a magnetically
shielded Hall thruster using internally and externally mounted cathodes. A numerical model …

Computer simulations of Hall thrusters without wall losses designed using two permanent magnetic rings

D Yongjie, P Wuji, W Liqiu, S Guoshun… - Journal of Physics D …, 2016 - iopscience.iop.org
A type of Hall thruster without wall losses is designed by adding two permanent magnet
rings in the magnetic circuit. The maximum strength of the magnetic field is set outside the …

Direct multipixel imaging and spectroscopy of an exoplanet with a solar gravity lens mission

SG Turyshev, M Shao, VT Toth, LD Friedman… - arXiv preprint arXiv …, 2020 - arxiv.org
We examined the solar gravitational lens (SGL) as the means to produce direct high-
resolution, multipixel images of exoplanets. The properties of the SGL are remarkable: it …

SmallSat missions enabled by paired low-thrust hybrid rocket and low-power long-life hall thruster

RW Conversano, J Rabinovitch… - 2019 IEEE …, 2019 - ieeexplore.ieee.org
The capabilities of a SmallSat-class spacecraft targeting the outer solar system and using a
combined chemical and electric propulsion system are explored. The development of …

[PDF][PDF] Development and initial performance testing of a low-power magnetically shielded Hall thruster with an internally-mounted hollow cathode

RW Conversano, RB Lobbia, KC Tilley… - 35th International …, 2017 - electricrocket.org
A new development model MaSMi Hall thruster, which utilizes a compact internally-mounted
hollow cathode, was designed, fabricated, and tested. The low-current cathode …