BOREALIS – Biofilm Onboard Radiation Exposure Assessment Lab In Space – is a 6U CubeSat mission developed under the Italian Space Agency’s ALCOR program. It introduces a dual-phase orbital profile enabling biological experimentation in both Low Earth Orbit (LEO) and Medium Earth Orbit (MEO), making BOREALIS one of the first CubeSat missions to attempt a LEO-to-MEO orbital transfer. This paper focuses on the mission’s engineering innovations that make this transfer feasible, particularly the propulsion subsystem based on a water-fueled pulsed plasma thruster and the Attitude Determination and Control System (ADCS), validated through numerical and Hardware-in-the-Loop (HIL) experiments. Conducted in collaboration between the School of Aerospace Engineering of Rome and the University of Arizona, the tests demonstrated that a commercial ADCS can maintain sub-degree pointing during long-duration thrust operations when integrated within a closed-loop Simulink environment.
Mission Design and Enabling Technologies for a LEO-to-MEO Dual-Phase CubeSat Mission: The BOREALIS Platform / Nardi, L., Curti, F., Carletta, S., Abbasrezaee, P., Contessa, L.T., Di Serafino, A., Omrani, V., Caputo, D., Palmerini, G., Lovecchio, N., Sriramoju, S., Siva Sankaram Emani, V.s., Burgio, N., Petrucci, G., Mazzotti, R., Mirasoli, M., Lorenzini, F., Mergé, M., Nascetti, A.. - (2025). (AIDAA International Congress 2025 Turin; Italy ).
Mission Design and Enabling Technologies for a LEO-to-MEO Dual-Phase CubeSat Mission: The BOREALIS Platform
Lorenzo Nardi;Fabio Curti;Stefano Carletta;Parsa Abbasrezaee;Lorenzo Thomas Contessa;A. Di Serafino;Vahid Omrani;Domenico Caputo;Giovanni Palmerini;Nicola Lovecchio;Sahithi Sriramoju;Nunzio Burgio;Giulia Petrucci;Fabio Lorenzini;Augusto Nascetti
2025
Abstract
BOREALIS – Biofilm Onboard Radiation Exposure Assessment Lab In Space – is a 6U CubeSat mission developed under the Italian Space Agency’s ALCOR program. It introduces a dual-phase orbital profile enabling biological experimentation in both Low Earth Orbit (LEO) and Medium Earth Orbit (MEO), making BOREALIS one of the first CubeSat missions to attempt a LEO-to-MEO orbital transfer. This paper focuses on the mission’s engineering innovations that make this transfer feasible, particularly the propulsion subsystem based on a water-fueled pulsed plasma thruster and the Attitude Determination and Control System (ADCS), validated through numerical and Hardware-in-the-Loop (HIL) experiments. Conducted in collaboration between the School of Aerospace Engineering of Rome and the University of Arizona, the tests demonstrated that a commercial ADCS can maintain sub-degree pointing during long-duration thrust operations when integrated within a closed-loop Simulink environment.| File | Dimensione | Formato | |
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Nardi_Mission Design_2025.pdf
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