PofoliaShared via Pofolia

CEAS Space Journal· 2026Q2

Propulsion and attitude control for Foresail-2: harnessing water electrolysis propulsion in a 6U CubeSat mission

Chiara Panozzo, Sascha Dengler, Sören Heizmann, Tomáš Mrázek et al.

Short summary

The Foresail-2 mission successfully demonstrates a Water Electrolysis Propulsion (WEP) system for attitude control and de-orbiting in a 6U CubeSat, overcoming limitations of conventional systems in Geostationary Transfer Orbit.

AI-generated from the title and abstract; the full text is not read.

Key points

  • Foresail-2 mission utilizes a Water Electrolysis Propulsion (WEP) system for attitude control and de-orbiting.
  • WEP produces hydrogen and oxygen propellants by electrolyzing onboard water.
  • The system is designed for precise attitude control and de-orbiting in Geostationary Transfer Orbit.
  • WEP offers high specific impulse, compact storage, and reduced power demands, aligning with sustainability standards.

AI-generated from the title and abstract; the full text is not read.

Abstract

Abstract The Foresail-2 mission, a 6U CubeSat developed by the Finnish Center of Excellence in Research of Sustainable Space, seeks to investigate ultra-low-frequency waves in the inner magnetosphere and validate innovative de-orbiting technologies. The mission’s demanding attitude control requirements, including sun-pointing spin axis stabilization and tether-assisted de-orbiting, pose significant challenges, particularly in Geostationary Transfer Orbit where conventional propulsion systems are ineffective. This paper introduces the Water Electrolysis Propulsion (WEP) system as a novel, green propulsion solution tailored to the mission’s needs. By electrolysing onboard water to produce hydrogen and oxygen propellants, WEP offers high specific impulse, compact storage and reduced power demands, while aligning with emerging sustainability standards. Through detailed analysis of system architecture, integration and performance, this paper demonstrates WEP’s potential to enable precise attitude control and de-orbiting for CubeSats, paving the way for scalable propulsion in future small satellite missions.

The authors' abstract, as published at the source. CEAS Space Journal, 2026 · DOI ↗

TakeawaysIn the app
Ask the paperIn the app

The rest is in the Pofolia app

Takeaways and questions to the paper; new summaries every day for your field. Free.

Sign in on the web to open

Field: Aerospace Engineering

Aerospace EngineeringEngineering