[HTML][HTML] LUMIO: A CubeSat for observing and characterizing micro-meteoroid impacts on the lunar far side

A Cervone, F Topputo, S Speretta, A Menicucci… - Acta Astronautica, 2022 - Elsevier
Abstract The Earth-Moon system is constantly bombarded by meteoroids of different size
and impact speed. Observation of the impacts on the Moon can enable thorough …

[PDF][PDF] Phase a design of the lumio spacecraft: a cubesat for observing and characterizing micro-meteoroid impacts on the lunar far side

A Cervone, F Topputo, S Speretta… - INTERNATIONAL …, 2020 - re.public.polimi.it
Abstract The LUnar Meteoroid Impacts Observer (LUMIO) is a CubeSat mission to a halo
orbit at Earth–Moon L2 that shall observe, quantify, and characterize meteoroid impacts on …

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

S Speretta, E Turan, A Cervone… - 2022 IEEE …, 2022 - ieeexplore.ieee.org
The Lunar Meteoroid Impact Observer (LUMIO) is a CubeSat mission at the Earth-Moon
Lagrangian point 2 (L 2) designed to observe, quantify, and characterize the meteoroid …

Design challenges and opportunities offered by the lumio spacecraft: a cubesat for observing and characterizing micro-meteoroid impacts on the lunar far side

A Cervone, F Topputo, S Speretta… - 72nd International …, 2021 - research.tudelft.nl
Delft University of Technology Design Challenges and Opportunities Offered by the LUMIO
Spacecraft a CubeSat for Observing and C Page 1 Delft University of Technology Design …

CubeSat Technology Past and Present: Current State-of-the-Art Survey

BMM Bomani - 2021 - ntrs.nasa.gov
A cube satellite (CubeSat) is an evolving and emerging technology that gives a novice or
advanced researcher relatively affordable access to space research experiments and …

Orbit maintenance strategy for libration point orbits. Floquet modes approach

S Cravedi - 2018 - politesi.polimi.it
The restricted three-body problem or RTBP, provides unique design solutions for space
applications, ranging from Lagrange point orbits to low energy transfers. In this scenario …

Selection of the Propulsion System for the LUMIO Mission: an Intricate Trade-Off Between Cost, Reliability and Performance

A Cervone, S Speretta, A Menicucci… - 72nd International …, 2021 - research.tudelft.nl
Abstract The Lunar Meteoroid Impact Observer (LUMIO), one of the two winning concepts of
the SysNova Lunar CubeSats for Exploration call by ESA, is a mission designed to observe …

[PDF][PDF] The Radiation Environment and effects analysis of the LUMIO Mission

A Menicucci, A Cervone, S Speretta… - INTERNATIONAL …, 2021 - re.public.polimi.it
Abstract The Lunar Meteoroid Impact Observer (LUMIO) is a mission designed to observe,
quantify, and characterise the impacts of meteoroids by detecting their flashes on the far side …

An analysis of attitude control laws and thruster configurations for a deep space CubeSat

MT Pinca - 2018 - politesi.polimi.it
CubeSats are a class of miniaturized satellites, originally developed in 1999 for academic
purposes. Their importance has grown with time, with several missions involving CubeSats …

[PDF][PDF] Modeling of Solar Array Drive Assembly (SADA) for LUMIO spacecraft

BF Nicola - 2020 - researchgate.net
The considered real system is the Lunar Meteoroid Impact Observer (LUMIO) spacecraft.
LUMIO is a CubeSat mission to a quasi-halo orbit at Earth–Moon L2 that shall observe …