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Swarm of lightsail nanosatellites for Solar System exploration

This paper presents a study for the realization of a space mission which employs nanosatellites driven by an external laser source impinging on an optimized lightsail, as a valuable technology to launch swarms of spacecrafts into the Solar System. Nanosatellites propelled by laser can be useful for...

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Autores principales: Santi, Giovanni, Corso, Alain J., Garoli, Denis, Lio, Giuseppe Emanuele, Manente, Marco, Favaro, Giulio, Bazzan, Marco, Piotto, Giampaolo, Andriolli, Nicola, Strambini, Lucanos, Pavarin, Daniele, Badia, Leonardo, Proietti Zaccaria, Remo, Lubin, Philip, Ragazzoni, Roberto, Pelizzo, Maria G.
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Nature Publishing Group UK 2023
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10638386/
https://www.ncbi.nlm.nih.gov/pubmed/37949919
http://dx.doi.org/10.1038/s41598-023-46101-3
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author Santi, Giovanni
Corso, Alain J.
Garoli, Denis
Lio, Giuseppe Emanuele
Manente, Marco
Favaro, Giulio
Bazzan, Marco
Piotto, Giampaolo
Andriolli, Nicola
Strambini, Lucanos
Pavarin, Daniele
Badia, Leonardo
Proietti Zaccaria, Remo
Lubin, Philip
Ragazzoni, Roberto
Pelizzo, Maria G.
author_facet Santi, Giovanni
Corso, Alain J.
Garoli, Denis
Lio, Giuseppe Emanuele
Manente, Marco
Favaro, Giulio
Bazzan, Marco
Piotto, Giampaolo
Andriolli, Nicola
Strambini, Lucanos
Pavarin, Daniele
Badia, Leonardo
Proietti Zaccaria, Remo
Lubin, Philip
Ragazzoni, Roberto
Pelizzo, Maria G.
author_sort Santi, Giovanni
collection PubMed
description This paper presents a study for the realization of a space mission which employs nanosatellites driven by an external laser source impinging on an optimized lightsail, as a valuable technology to launch swarms of spacecrafts into the Solar System. Nanosatellites propelled by laser can be useful for heliosphere exploration and for planetary observation, if suitably equipped with sensors, or be adopted for the establishment of network systems when placed into specific orbits. By varying the area-to-mass ratio (i.e. the ratio between the sail area and the payload weight) and the laser power, it is possible to insert nanosatellites into different hyperbolic orbits with respect to Earth, thus reaching the target by means of controlled trajectories in a relatively short amount of time. A mission involving nanosatellites of the order of 1 kg of mass is envisioned, by describing all the on-board subsystems and satisfying all the requirements in terms of power and mass budget. Particular attention is paid to the telecommunication subsystem, which must offer all the necessary functionalities. To fabricate the lightsail, the thin films technology has been considered, by verifying the sail’s thermal stability during the thrust phase. Moreover, the problem of mechanical stability of the lightsail has been tackled, showing that the distance between the ligthsail structure and the payload plays a pivotal role. Some potential applications of the proposed technology are discussed, such as the mapping of the heliospheric environment.
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spelling pubmed-106383862023-11-11 Swarm of lightsail nanosatellites for Solar System exploration Santi, Giovanni Corso, Alain J. Garoli, Denis Lio, Giuseppe Emanuele Manente, Marco Favaro, Giulio Bazzan, Marco Piotto, Giampaolo Andriolli, Nicola Strambini, Lucanos Pavarin, Daniele Badia, Leonardo Proietti Zaccaria, Remo Lubin, Philip Ragazzoni, Roberto Pelizzo, Maria G. Sci Rep Article This paper presents a study for the realization of a space mission which employs nanosatellites driven by an external laser source impinging on an optimized lightsail, as a valuable technology to launch swarms of spacecrafts into the Solar System. Nanosatellites propelled by laser can be useful for heliosphere exploration and for planetary observation, if suitably equipped with sensors, or be adopted for the establishment of network systems when placed into specific orbits. By varying the area-to-mass ratio (i.e. the ratio between the sail area and the payload weight) and the laser power, it is possible to insert nanosatellites into different hyperbolic orbits with respect to Earth, thus reaching the target by means of controlled trajectories in a relatively short amount of time. A mission involving nanosatellites of the order of 1 kg of mass is envisioned, by describing all the on-board subsystems and satisfying all the requirements in terms of power and mass budget. Particular attention is paid to the telecommunication subsystem, which must offer all the necessary functionalities. To fabricate the lightsail, the thin films technology has been considered, by verifying the sail’s thermal stability during the thrust phase. Moreover, the problem of mechanical stability of the lightsail has been tackled, showing that the distance between the ligthsail structure and the payload plays a pivotal role. Some potential applications of the proposed technology are discussed, such as the mapping of the heliospheric environment. Nature Publishing Group UK 2023-11-09 /pmc/articles/PMC10638386/ /pubmed/37949919 http://dx.doi.org/10.1038/s41598-023-46101-3 Text en © The Author(s) 2023 https://creativecommons.org/licenses/by/4.0/Open Access This article is licensed under a Creative Commons Attribution 4.0 International License, which permits use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons licence, and indicate if changes were made. The images or other third party material in this article are included in the article’s Creative Commons licence, unless indicated otherwise in a credit line to the material. If material is not included in the article’s Creative Commons licence and your intended use is not permitted by statutory regulation or exceeds the permitted use, you will need to obtain permission directly from the copyright holder. To view a copy of this licence, visit http://creativecommons.org/licenses/by/4.0/ (https://creativecommons.org/licenses/by/4.0/) .
spellingShingle Article
Santi, Giovanni
Corso, Alain J.
Garoli, Denis
Lio, Giuseppe Emanuele
Manente, Marco
Favaro, Giulio
Bazzan, Marco
Piotto, Giampaolo
Andriolli, Nicola
Strambini, Lucanos
Pavarin, Daniele
Badia, Leonardo
Proietti Zaccaria, Remo
Lubin, Philip
Ragazzoni, Roberto
Pelizzo, Maria G.
Swarm of lightsail nanosatellites for Solar System exploration
title Swarm of lightsail nanosatellites for Solar System exploration
title_full Swarm of lightsail nanosatellites for Solar System exploration
title_fullStr Swarm of lightsail nanosatellites for Solar System exploration
title_full_unstemmed Swarm of lightsail nanosatellites for Solar System exploration
title_short Swarm of lightsail nanosatellites for Solar System exploration
title_sort swarm of lightsail nanosatellites for solar system exploration
topic Article
url https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10638386/
https://www.ncbi.nlm.nih.gov/pubmed/37949919
http://dx.doi.org/10.1038/s41598-023-46101-3
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