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High-order moment models and multi-scale numerical methods for plasmas applied to electric propulsion

Project description

Enabling improved and cheaper electric propulsion thrusters

The rising need for small satellites, which are less expensive to launch and can create constellations, has led to progress in propulsion tech. Electric propulsion (EP) is a key innovation as it gives a long operational life, lower costs, and accurate thrust control. Yet, EP has problems, such as costly and limited propellants and a long creation period, mostly from not having models that correctly show the complex plasma physics involved. The ERC-funded HiMomPlas project aims to create better predictive plasma models. These models will allow the making of thrusters that have improved performance, stability, and lower costs, while also giving key information on how long they last.

Objective

We are in the midst of a technological revolution characterized by the large demand for small satellites. These satellites are cheaper to launch and allow for forming constellations, impossible with larger satellites. As a result, they require propulsion systems in order to control their trajectories. Electric propulsion (EP) largely reduces the operational costs, using less propellant, precisely controlling thrust, and operating for long times. The response to the demand for EP is currently at stake because of two reasons: 1) Most of the thrusters operate with an expensive and scarce propellant gas, xenon, and 2) The development of the engines follows an empirical approach that is long and expensive, which limits the optimization and conception of new prototypes. These limitations are due to the lack of models that capture the complex plasma physics in EP, in particular: 1) The impact of the plasma composition and thruster geometry on the performance, 2) The presence of multi-scale plasma kinetic instabilities, and 3) The erosion of the walls interacting with the plasma.
Our objective is to develop advanced predictive plasma models, able to help to the conception of new thrusters operating with cheaper propellants, improving their stability and performance, and predicting their lifetime, without the need of expensive experimental campaigns. We will follow a multidisciplinary approach, integrating physicist, engineers, chemists, and applied mathematicians. Our methodology aims at extending the classical fluid equations by solving for higher-order moments, allowing to describe in an efficient manner microscopic (kinetic) processes. With advanced numerical techniques, we will propose multi-scale models able to describe the turbulent phenomena, the wall processes, and efficiently simulate the multi-scale nature of EP. The models will be integrated into a numerical tool that will be validated with experiments using cutting-edge uncertainty quantification techniques.

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(opens in new window) ERC-2025-STG

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Host institution

CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE CNRS
Net EU contribution

Net EU financial contribution. The sum of money that the participant receives, deducted by the EU contribution to its linked third party. It considers the distribution of the EU financial contribution between direct beneficiaries of the project and other types of participants, like third-party participants.

€ 1 499 951,00
Address
RUE MICHEL ANGE 3
75794 PARIS
France

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Region
Ile-de-France Ile-de-France Paris
Activity type
Research Organisations
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Total cost

The total costs incurred by this organisation to participate in the project, including direct and indirect costs. This amount is a subset of the overall project budget.

€ 1 499 951,00

Beneficiaries (1)

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