[HTML][HTML] Space micropropulsion systems for Cubesats and small satellites: From proximate targets to furthermost frontiers

I Levchenko, K Bazaka, Y Ding, Y Raitses… - Applied Physics …, 2018 - pubs.aip.org
Rapid evolution of miniaturized, automatic, robotized, function-centered devices has
redefined space technology, bringing closer the realization of most ambitious interplanetary …

An overview of cube-satellite propulsion technologies and trends

AR Tummala, A Dutta - Aerospace, 2017 - mdpi.com
CubeSats provide a cost effective means to perform scientific and technological studies in
space. Due to their affordability, CubeSat technologies have been diversely studied and …

Emission characteristics of passively fed electrospray microthrusters with propellant reservoirs

D Krejci, F Mier-Hicks, R Thomas, T Haag… - Journal of Spacecraft …, 2017 - arc.aiaa.org
The characterization of a miniaturized ionic liquid electrospray thruster for nanosatellite
applications is presented. The thruster investigated features an emitter array of 480 emitter …

[HTML][HTML] The role of secondary species emission in vacuum facility effects for electrospray thrusters

NM Uchizono, AL Collins, C Marrese-Reading… - Journal of Applied …, 2021 - pubs.aip.org
Theoretical, analytical, and experimental investigations of electrospray operation in vacuum
facilities show that secondary species emission (SSE) plays a significant role in the behavior …

Fabrication and characterization of a fully conventionally machined, high-performance porous-media electrospray thruster

MR Natisin, HL Zamora, WA McGehee… - Journal of …, 2020 - iopscience.iop.org
While electrospray devices have been used in a variety of applications for decades, they
have recently seen a surge in research within the field of electric propulsion. These research …

Lifetime considerations for electrospray thrusters

A Thuppul, PL Wright, AL Collins, JK Ziemer, RE Wirz - Aerospace, 2020 - mdpi.com
Ionic liquid electrospray thrusters are capable of producing microNewton precision thrust at
a high thrust–power ratio but have yet to demonstrate lifetimes that are suitable for most …

[HTML][HTML] Direct thrust test and asymmetric performance of porous ionic liquid electrospray thruster

GUO Yuntao, SUN Wei, SUN Zhenning… - Chinese Journal of …, 2023 - Elsevier
In order to meet the demand of CubeSats for low power and high-performance micro-
propulsion system, a porous ionic liquid electrospray thruster prototype is developed in this …

A review of MEMS micropropulsion technologies for CubeSats and PocketQubes

MAC Silva, DC Guerrieri, A Cervone, E Gill - Acta Astronautica, 2018 - Elsevier
CubeSats have been extensively used in the past decade as scientific tools, technology
demonstrators and for education. Recently, PocketQubes have emerged as an interesting …

Efficiency mechanisms in porous-media electrospray thrusters

MR Natisin, HL Zamora, ZA Holley… - Journal of propulsion …, 2021 - arc.aiaa.org
The overall propulsion efficiency for ion-mode electrospray thrusters has been predicted to
be as high as 90%; however, experimental measurements currently fall far short of these …

Emission modes in electrospray thrusters operating with high conductivity ionic liquids

NM Uchizono, AL Collins, A Thuppul, PL Wright… - Aerospace, 2020 - mdpi.com
Electrospray thruster life and mission performance are strongly influenced by grid
impingement, the extent of which can be correlated with emission modes that occur at …