Ion thrusters for electric propulsion: Scientific issues developing a niche technology into a game changer
K Holste, P Dietz, S Scharmann, K Keil… - Review of Scientific …, 2020 - pubs.aip.org
The transition from old space to new space along with increasing commercialization has a
major impact on space flight, in general, and on electric propulsion (EP) by ion thrusters, in …
major impact on space flight, in general, and on electric propulsion (EP) by ion thrusters, in …
Faraday cup sizing for electric propulsion ion beam study: Case of a field-emission-electric propulsion thruster
V Hugonnaud, S Mazouffre, D Krejci - Review of Scientific Instruments, 2021 - pubs.aip.org
This article provides information about the sizing and standardization of a Faraday cup (FC)
used as a plasma diagnostic. This instrument is used to accurately map the ion beam profile …
used as a plasma diagnostic. This instrument is used to accurately map the ion beam profile …
Characterization of film-evaporating microcapillaries for water-based microthrusters
S Pugia, A Cofer, A Alexeenko - Acta Astronautica, 2022 - Elsevier
Compact micronewton thrusters can provide attitude control for small satellites to increase
mission duration and enable constellation flying. Micronewton thrust control can also …
mission duration and enable constellation flying. Micronewton thrust control can also …
[PDF][PDF] The first 100 FEEP propulsion systems in space: A statistical view and lessons learnt of 4 years of ENPULSION
D Krejci, A Reissner - … Institute of Technology, Cambridge, MA USA, 2022 - enpulsion.com
After launch in Dec 2018, the first propulsion system based on liquid metal Field Emission
Electric Propulsion (FEEP) was successfully demonstrated in orbit in 2019 in an IOD …
Electric Propulsion (FEEP) was successfully demonstrated in orbit in 2019 in an IOD …
Improving the performance of a water ion thruster using biased electrodes
Y Ataka, Y Nakagawa, H Koizumi, K Komurasaki - Acta Astronautica, 2021 - Elsevier
This paper investigates whether biased electrodes can improve the performance of a
microwave-discharge water ion thruster, which has been proposed as a propulsion system …
microwave-discharge water ion thruster, which has been proposed as a propulsion system …
138 Propulsion Units Launched in 4 Years: A Review and Lessons Learned
D Krejci, A Reissner - 2022 - digitalcommons.usu.edu
After the first launch of an ENPULSION NANO thruster in 2019 together with FOTEC1, 2, 3,
which verified for the first time the operation of a propulsion system based on liquid metal …
which verified for the first time the operation of a propulsion system based on liquid metal …
Large number system integration aspects: on orbit data and lessons learnt from launching 144 FEEP propulsion systems
D Krejci, A Reissner - Journal of Electric Propulsion, 2022 - Springer
This manuscript discusses the on orbit data availability and system integration aspects of the
ENPULSION NANO liquid metal FEEP propulsion systems. We present flight data from …
ENPULSION NANO liquid metal FEEP propulsion systems. We present flight data from …
Low-earth-orbit constellation phasing using miniaturized low-thrust propulsion systems
T Lafleur, N Apffel - Journal of Spacecraft and Rockets, 2021 - arc.aiaa.org
Many low-Earth-orbit constellations consist of multiple small satellites that are launched
together in batches, and which make use of differential atmospheric drag for subsequent …
together in batches, and which make use of differential atmospheric drag for subsequent …
Fully discrete model of kinetic ion-induced electron emission from metal surfaces
Ion-induced electron emission (IIEE) is an important process whereby ions impinging on a
material surface lead to net emission of electrons into the vacuum. While relevant for …
material surface lead to net emission of electrons into the vacuum. While relevant for …
Ion-induced electron emission by keV-range energy indium ions: Influence of material and geometry
V Hugonnaud, S Mazouffre, D Krejci - Journal of Applied Physics, 2022 - pubs.aip.org
This work provides measurements of the ion-induced electron emission yield caused by keV-
range energy indium ions (3–8 keV). In our experiment, the ion sources, fueled with indium …
range energy indium ions (3–8 keV). In our experiment, the ion sources, fueled with indium …