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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...
Autores principales: | , , , , , , , , , , , , , , , |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
Nature Publishing Group UK
2023
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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. |
format | Online Article Text |
id | pubmed-10638386 |
institution | National Center for Biotechnology Information |
language | English |
publishDate | 2023 |
publisher | Nature Publishing Group UK |
record_format | MEDLINE/PubMed |
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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