_version_ 1866908567818207232
author Lombardi, Giovanni
Fabiani, Sergio
Del Monte, Ettore
Alimenti, Andrea
Campana, Riccardo
Centrone, Mauro
Costa, Enrico
De Angelis, Nicolas
De Cesare, Giovanni
Di Cosimo, Sergio
Di Persio, Giuseppe
Kumar, Abhay
Lacerenza, Alessandro
Loffredo, Pasqualino
Minervini, Gabriele
Muleri, Fabio
Romano, Paolo
Rubini, Alda
Scalise, Emanuele
Silva, Enrico
Soffitta, Paolo
Albanesi, Davide
Baffo, Ilaria
Brienza, Daniele
Campamaggiore, Valerio
Cucinella, Giovanni
Curatolo, Andrea
de Iulis, Giulia
Del Re, Andrea
Di Bari, Vito
Di Filippo, Simone
Donnarumma, Immacolata
Fanelli, Pierluigi
Gagliardi, Nicolas
Leonetti, Paolo
Merge, Matteo
Modenini, Dario
Negri, Andrea
Pecorella, Daniele
Perelli, Massimo
Ponti, Alice
Sbop, Francesca
Tortora, Paolo
Turchi, Alessandro
Vagelli, Valerio
Zaccagnino, Emanuele
Zambardi, Alessandro
Zazza, Costantino
author_facet Lombardi, Giovanni
Fabiani, Sergio
Del Monte, Ettore
Alimenti, Andrea
Campana, Riccardo
Centrone, Mauro
Costa, Enrico
De Angelis, Nicolas
De Cesare, Giovanni
Di Cosimo, Sergio
Di Persio, Giuseppe
Kumar, Abhay
Lacerenza, Alessandro
Loffredo, Pasqualino
Minervini, Gabriele
Muleri, Fabio
Romano, Paolo
Rubini, Alda
Scalise, Emanuele
Silva, Enrico
Soffitta, Paolo
Albanesi, Davide
Baffo, Ilaria
Brienza, Daniele
Campamaggiore, Valerio
Cucinella, Giovanni
Curatolo, Andrea
de Iulis, Giulia
Del Re, Andrea
Di Bari, Vito
Di Filippo, Simone
Donnarumma, Immacolata
Fanelli, Pierluigi
Gagliardi, Nicolas
Leonetti, Paolo
Merge, Matteo
Modenini, Dario
Negri, Andrea
Pecorella, Daniele
Perelli, Massimo
Ponti, Alice
Sbop, Francesca
Tortora, Paolo
Turchi, Alessandro
Vagelli, Valerio
Zaccagnino, Emanuele
Zambardi, Alessandro
Zazza, Costantino
contents The space-based CUbesat Solar Polarimeter (CUSP) mission aims to measure the linear polarization of solar flares in the hard X-ray band by means of a Compton scattering polarimeter. CUSP is a project in the framework of the Alcor Program of the Italian Space Agency aimed at developing new CubeSat missions. As part of CUSP's Phase B study, which began in December 2024 and will last one year, we present the current development status of the design solutions adopted for the mission's most critical multi-physics design drivers. These solutions have been formulated and applied to demonstrate compliance with system requirements at both the spacecraft and platform levels. In particular, we describe the mechanical design of each structural component, the results of static, dynamic finite element analyses, and a proposal for topological optimization of the interface between the platform and payload and some fixture for test, and the preliminary environmental testing campaign (e.g., vibration, shock) that will be carried out on a mechanical demonstrator.
format Preprint
id arxiv_https___arxiv_org_abs_2508_02594
institution arXiv
publishDate 2025
record_format arxiv
spellingShingle The multi-physics analysis, design and testing of CUSP, a CubeSat mission for space weather and solar flares x-ray polarimetry
Lombardi, Giovanni
Fabiani, Sergio
Del Monte, Ettore
Alimenti, Andrea
Campana, Riccardo
Centrone, Mauro
Costa, Enrico
De Angelis, Nicolas
De Cesare, Giovanni
Di Cosimo, Sergio
Di Persio, Giuseppe
Kumar, Abhay
Lacerenza, Alessandro
Loffredo, Pasqualino
Minervini, Gabriele
Muleri, Fabio
Romano, Paolo
Rubini, Alda
Scalise, Emanuele
Silva, Enrico
Soffitta, Paolo
Albanesi, Davide
Baffo, Ilaria
Brienza, Daniele
Campamaggiore, Valerio
Cucinella, Giovanni
Curatolo, Andrea
de Iulis, Giulia
Del Re, Andrea
Di Bari, Vito
Di Filippo, Simone
Donnarumma, Immacolata
Fanelli, Pierluigi
Gagliardi, Nicolas
Leonetti, Paolo
Merge, Matteo
Modenini, Dario
Negri, Andrea
Pecorella, Daniele
Perelli, Massimo
Ponti, Alice
Sbop, Francesca
Tortora, Paolo
Turchi, Alessandro
Vagelli, Valerio
Zaccagnino, Emanuele
Zambardi, Alessandro
Zazza, Costantino
Instrumentation and Methods for Astrophysics
Solar and Stellar Astrophysics
Space Physics
The space-based CUbesat Solar Polarimeter (CUSP) mission aims to measure the linear polarization of solar flares in the hard X-ray band by means of a Compton scattering polarimeter. CUSP is a project in the framework of the Alcor Program of the Italian Space Agency aimed at developing new CubeSat missions. As part of CUSP's Phase B study, which began in December 2024 and will last one year, we present the current development status of the design solutions adopted for the mission's most critical multi-physics design drivers. These solutions have been formulated and applied to demonstrate compliance with system requirements at both the spacecraft and platform levels. In particular, we describe the mechanical design of each structural component, the results of static, dynamic finite element analyses, and a proposal for topological optimization of the interface between the platform and payload and some fixture for test, and the preliminary environmental testing campaign (e.g., vibration, shock) that will be carried out on a mechanical demonstrator.
title The multi-physics analysis, design and testing of CUSP, a CubeSat mission for space weather and solar flares x-ray polarimetry
topic Instrumentation and Methods for Astrophysics
Solar and Stellar Astrophysics
Space Physics
url https://arxiv.org/abs/2508.02594