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Smart Micronozzles for Next-Generation Supercritical Fluid-Based Microthrusters

Project description

Compact, high-performance propulsion systems for small satellites

Small satellites and CubeSats have opened new possibilities for affordable and versatile space missions, from Earth observation to communication networks. However, their propulsion systems present challenges including low thrust, poor scalability and integration with the compact design of these satellites. Smart supercritical fluid-based micronozzles (SSFMs) offer a breakthrough solution. These miniaturised propulsion units use high-energy, non-toxic fluids to enable fine attitude control and high-agility manoeuvres. Compared to current systems, SSFMs promise up to five times higher thrust density, reduced weight by 20 % and smaller volume by 30 %. The ERC-funded STELLAR project plans to develop and test such prototypes under realistic conditions. The project will target a final technology readiness level of 4. Beyond space, SSFMs could also impact biomedical microfluidics and robotics.

Objective

The STELLAR project aims to demonstrate the proof-of-concept for a novel micropropulsion technology —Smart Supercritical Fluid-Based Micronozzles (SSFMs)— designed to meet the growing needs of CubeSats and small satellites. These miniaturized propulsion units will use supercritical fluids to deliver compact, efficient, and tunable thrust, addressing critical limitations in current systems, such as low thrust density, poor scalability, and integration complexity. SSFMs combine advanced microfabrication, integrated sensor control, and real-time flow modulation to enable both fine attitude control and high-agility maneuvers using non-toxic, high-energy fluids. Compared to state-of-the-art cold-gas or electrothermal thrusters, SSFMs are expected to deliver up to 5x higher thrust density, reduce volume by up to 30%, and cut weight by up to 20%, while also enhancing responsiveness and system autonomy. Building on results from the ERC-funded SCRAMBLE project, STELLAR will fabricate and test functional SSFM prototypes under representative pressure and thermal conditions, validating key performance metrics including thrust, impulse, and flow stability. The project will target a final technology readiness level (TRL) of 4, representing laboratory validation of the integrated prototype. Supporting activities include advanced simulations for micronozzle optimization, stakeholder engagement, and intellectual property protection. In parallel, the SSFM architecture offers cross-sector potential in biomedical microfluidics, electronics cooling, and soft robotics; domains that share similar demands for compact, thermally efficient fluidic control. By addressing both space and cross-sector challenges, STELLAR will bridge the gap between advanced microfluidics research and next-generation space technologies, enabling more agile, sustainable, and mission-adaptive propulsion for small spacecraft.

Programme(s)

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Topic(s)

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Funding Scheme

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HORIZON-ERC-POC - HORIZON ERC Proof of Concept Grants

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Call for proposal

Procedure for inviting applicants to submit project proposals, with the aim of receiving EU funding.

(opens in new window) ERC-2025-POC

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Host institution

UNIVERSITAT POLITECNICA DE CATALUNYA
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.

€ 150 000,00
Address
CALLE JORDI GIRONA 31
08034 BARCELONA
Spain

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Region
Este Cataluña Barcelona
Activity type
Higher or Secondary Education Establishments
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Total cost

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Beneficiaries (1)

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