LUMIO: A CubeSat to Monitor Micro-meteroid Impacts on the Lunar Farside

Conference Paper (2022)
Author(s)

E. Turan (TU Delft - Space Systems Egineering)

S. Speretta (TU Delft - Space Systems Egineering)

A. Cervone (TU Delft - Space Systems Egineering)

A. Menicucci (TU Delft - Space Systems Egineering)

Francesco Topputo (Politecnico di Milano)

Vittorio Franzese (Politecnico di Milano)

Carmine Giordano (Politecnico di Milano)

Gianmario Merisio (Politecnico di Milano)

Pierluigi Di Lizia (Politecnico di Milano)

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DOI related publication
https://doi.org/10.1109/AERO53065.2022.9843311 Final published version
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Publication Year
2022
Language
English
Bibliographical Note
Green Open Access added to TU Delft Institutional Repository ‘You share, we take care!’ – Taverne project https://www.openaccess.nl/en/you-share-we-take-care Otherwise as indicated in the copyright section: the publisher is the copyright holder of this work and the author uses the Dutch legislation to make this work public.
ISBN (print)
978-1-6654-3760-8
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Abstract

The Lunar Meteoroid Impact Observer (LUMIO) is a CubeSat mission at the Earth-Moon Lagrangian point 2 (L2) designed to observe, quantify, and characterize the meteoroid impacts by detecting their flashes on the Lunar farside. LUMIO can be deployed as one of the payloads in the NASA Commercial Lunar Payload System or from Artemis-2 mission to a low Lunar orbit and to demonstrate autonomous navigation capabilities to reach its operational orbit around the Earth-Moon L2. From there, its scientific mission to map and investigate the spatial and temporal characteristics of meteoroids impacting the Lunar surface will start and is expected to last for one year. LUMIO is a 12U CubeSat including a dedicated camera to monitor impact flashes in the visible and near-infrared spectrum, and also allows estimating the impact of temperature and energy. Optical navigation using the payload camera will also demonstrate increased on-board autonomy and drastically reduced mission costs. Navigation validation will be carried out using standard ground-based radiometric techniques enabled by a miniaturized X-band coherent transponder on-board. LUMIO can also use an inter-satellite link for telemetry and control via a commercial Lunar data relay system, providing a redundant communication system and lowering the need for high-gain ground stations for routine operations. The satellite bus derives from a commercial version designed for Low Earth Orbit and it will feature several improvements to operate in the Lunar environment, including a more advanced thermal control and radiation shielding. Commercial Off-The-Shelf systems will require a radiation screening and this will contribute to maintain the mission budget low and aim at a launch date in 2024.

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