Computational modelling of water-fuelled Hall Effect Thrusters

Abstract This paper presents a Particle-In-Cell code designed for the simulation of water-fuelled Hall Effect Thrusters, including two different propellants: water vapour and oxygen (the latter being intended for water electrolysis propulsion with oxygen supplied through the anode and hydrogen through the cathode). The reactive model is structured in two stages, encompassing not only the initial reactions of water vapour and oxygen molecules ( $$1^{\textrm{st}}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mrow> <mml:msup> <mml:mn>1</mml:mn> <mml:mrow> <mml:mi>st</mml:mi> </mml:mrow> </mml:msup> </mml:mrow> </mml:math> stage) but also the reactions of the diatomic and monoatomic products resulting from them ( $$2^{\textrm{nd}}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mrow> <mml:msup> <mml:mn>2</mml:mn> <mml:mrow> <mml:mi>nd</mml:mi> </mml:mrow> </mml:msup> </mml:mrow> </mml:math> stage). Specifically, the model accounts for 45 reactions in the case of water vapour and 18 reactions in the case of oxygen, including the most relevant excitation events for each species. The Particle-In-Cell code uses a combination of a 0-dimensional model with a 2-dimensional model. The 0-dimensional model provides initial neutral and electron densities, as well as the most significant reactions, to facilitate the convergence of the 2-dimensional model without the computational burden of starting a simulation from scratch. The 0-dimensional model reveals that the reactions considered within the $$2^{\textrm{nd}}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mrow> <mml:msup> <mml:mn>2</mml:mn> <mml:mrow> <mml:mi>nd</mml:mi> </mml:mrow> </mml:msup> </mml:mrow> </mml:math> stage are crucial for the plasma species composition of the discharge. The oxygen plasmas consist mainly of O $$^{+}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow/> <mml:mo>+</mml:mo> </mml:mmultiscripts> </mml:math> and O $$_{2}^{+}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow> <mml:mn>2</mml:mn> </mml:mrow> <mml:mo>+</mml:mo> </mml:mmultiscripts> </mml:math> ions in a similar proportion, while double and negative ions do not play a significant role. Neutrals (O $$_2$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mn>2</mml:mn> <mml:mrow/> </mml:mmultiscripts> </mml:math> and O) also show similar distributions, depending on the thruster’s operating conditions. Water vapour plasmas are dominated by OH $$^{+}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow/> <mml:mo>+</mml:mo> </mml:mmultiscripts> </mml:math> , H $$_{2}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mn>2</mml:mn> <mml:mrow/> </mml:mmultiscripts> </mml:math> O $$^{+}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow/> <mml:mo>+</mml:mo> </mml:mmultiscripts> </mml:math> , H $$^{+}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow/> <mml:mo>+</mml:mo> </mml:mmultiscripts> </mml:math> , and O $$^{+}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow/> <mml:mo>+</mml:mo> </mml:mmultiscripts> </mml:math> ions, with other species such as H $$_{2}^{+}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow> <mml:mn>2</mml:mn> </mml:mrow> <mml:mo>+</mml:mo> </mml:mmultiscripts> </mml:math> , O $$^{++}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow/> <mml:mrow> <mml:mo>+</mml:mo> <mml:mo>+</mml:mo> </mml:mrow> </mml:mmultiscripts> </mml:math> , and negative ions being negligible. The neutral population is predominantly composed of monoatomic H particles. The 0-dimensional model also demonstrates that all ionisation fractions of the species follow an exponentially increasing trend with the electron temperature. Finally, the 2-dimensional model provides additional insight into the plasma evolution, electron temperature, power losses coming from the reactive model and equilibrium points of the system.

Authors

Institutions

Publication Details

Journal
Journal of Electric Propulsion
Published
2025-04-24
DOI
https://doi.org/10.1007/s44205-025-00124-2
Citations
2
Primary Topic
Plasma Diagnostics and Applications
Type
article
Field-Weighted Citation Impact
1.46

Funders

Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Computational modelling of water-fuelled Hall Effect Thrusters

J. Tejeda, Aaron Knoll, Jesús Perales-Díaz
2 citations
Journal of Electric Propulsion
Plasma Diagnostics and Applications
1.46
article

Computational modelling of water-fuelled Hall Effect Thrusters

J. Tejeda, Aaron Knoll, Jesús Perales-Díaz
article en
2 citations

Abstract

Abstract This paper presents a Particle-In-Cell code designed for the simulation of water-fuelled Hall Effect Thrusters, including two different propellants: water vapour and oxygen (the latter being intended for water electrolysis propulsion with oxygen supplied through the anode and hydrogen through the cathode). The reactive model is structured in two stages, encompassing not only the initial reactions of water vapour and oxygen molecules ( $$1^{\textrm{st}}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mrow> <mml:msup> <mml:mn>1</mml:mn> <mml:mrow> <mml:mi>st</mml:mi> </mml:mrow> </mml:msup> </mml:mrow> </mml:math> stage) but also the reactions of the diatomic and monoatomic products resulting from them ( $$2^{\textrm{nd}}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mrow> <mml:msup> <mml:mn>2</mml:mn> <mml:mrow> <mml:mi>nd</mml:mi> </mml:mrow> </mml:msup> </mml:mrow> </mml:math> stage). Specifically, the model accounts for 45 reactions in the case of water vapour and 18 reactions in the case of oxygen, including the most relevant excitation events for each species. The Particle-In-Cell code uses a combination of a 0-dimensional model with a 2-dimensional model. The 0-dimensional model provides initial neutral and electron densities, as well as the most significant reactions, to facilitate the convergence of the 2-dimensional model without the computational burden of starting a simulation from scratch. The 0-dimensional model reveals that the reactions considered within the $$2^{\textrm{nd}}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mrow> <mml:msup> <mml:mn>2</mml:mn> <mml:mrow> <mml:mi>nd</mml:mi> </mml:mrow> </mml:msup> </mml:mrow> </mml:math> stage are crucial for the plasma species composition of the discharge. The oxygen plasmas consist mainly of O $$^{+}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow/> <mml:mo>+</mml:mo> </mml:mmultiscripts> </mml:math> and O $$_{2}^{+}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow> <mml:mn>2</mml:mn> </mml:mrow> <mml:mo>+</mml:mo> </mml:mmultiscripts> </mml:math> ions in a similar proportion, while double and negative ions do not play a significant role. Neutrals (O $$_2$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mn>2</mml:mn> <mml:mrow/> </mml:mmultiscripts> </mml:math> and O) also show similar distributions, depending on the thruster’s operating conditions. Water vapour plasmas are dominated by OH $$^{+}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow/> <mml:mo>+</mml:mo> </mml:mmultiscripts> </mml:math> , H $$_{2}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mn>2</mml:mn> <mml:mrow/> </mml:mmultiscripts> </mml:math> O $$^{+}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow/> <mml:mo>+</mml:mo> </mml:mmultiscripts> </mml:math> , H $$^{+}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow/> <mml:mo>+</mml:mo> </mml:mmultiscripts> </mml:math> , and O $$^{+}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow/> <mml:mo>+</mml:mo> </mml:mmultiscripts> </mml:math> ions, with other species such as H $$_{2}^{+}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow> <mml:mn>2</mml:mn> </mml:mrow> <mml:mo>+</mml:mo> </mml:mmultiscripts> </mml:math> , O $$^{++}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow/> <mml:mrow> <mml:mo>+</mml:mo> <mml:mo>+</mml:mo> </mml:mrow> </mml:mmultiscripts> </mml:math> , and negative ions being negligible. The neutral population is predominantly composed of monoatomic H particles. The 0-dimensional model also demonstrates that all ionisation fractions of the species follow an exponentially increasing trend with the electron temperature. Finally, the 2-dimensional model provides additional insight into the plasma evolution, electron temperature, power losses coming from the reactive model and equilibrium points of the system.

Journal of Electric PropulsionVol. 4(1)
Jet Propulsion Laboratory (US), Imperial College London (GB), Universidad Carlos III de Madrid (ES)
European Space Agency
Openalex Percentile: Top 18%
Plasma Diagnostics and Applications
1.46
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.