_version_ 1866929410360213504
author Lombardi, Giovanni
Fabiani, Sergio
Del Monte, Ettore
Costa, Enrico
Soffitta, Paolo
Muleri, Fabio
Baffo, Ilaria
Biancolini, Marco E.
Bonomo, Sergio
Brienza, Daniele
Campana, Riccardo
Centrone, Mauro
Contini, Gessica
Cucinella, Giovanni
Curatolo, Andrea
De Angelis, Nicolas
De Cesare, Giovanni
Del Re, Andrea
Di Cosimo, Sergio
Di Filippo, Simone
Di Marco, Alessandro
Di Meo, Emanuele
Di Persio, Giuseppe
Donnarumma, Immacolata
Fanelli, Pierluigi
Leonetti, Paolo
Locarini, Alfredo
Loffredo, Pasqualino
Lopez, Andrea
Minervini, Gabriele
Modenini, Dario
Natalucci, Silvia
Negri, Andrea
Perelli, Massimo
Rossi, Monia
Rubini, Alda
Scalise, Emanuele
Terracciano, Andrea
Tortora, Paolo
Zaccagnino, Emanuele
Zambardi, Alessandro
author_facet Lombardi, Giovanni
Fabiani, Sergio
Del Monte, Ettore
Costa, Enrico
Soffitta, Paolo
Muleri, Fabio
Baffo, Ilaria
Biancolini, Marco E.
Bonomo, Sergio
Brienza, Daniele
Campana, Riccardo
Centrone, Mauro
Contini, Gessica
Cucinella, Giovanni
Curatolo, Andrea
De Angelis, Nicolas
De Cesare, Giovanni
Del Re, Andrea
Di Cosimo, Sergio
Di Filippo, Simone
Di Marco, Alessandro
Di Meo, Emanuele
Di Persio, Giuseppe
Donnarumma, Immacolata
Fanelli, Pierluigi
Leonetti, Paolo
Locarini, Alfredo
Loffredo, Pasqualino
Lopez, Andrea
Minervini, Gabriele
Modenini, Dario
Natalucci, Silvia
Negri, Andrea
Perelli, Massimo
Rossi, Monia
Rubini, Alda
Scalise, Emanuele
Terracciano, Andrea
Tortora, Paolo
Zaccagnino, Emanuele
Zambardi, Alessandro
contents The CUbesat Solar Polarimeter (CUSP) project aims to develop a constellation of two CubeSats orbiting the Earth to measure the linear polarization of solar flares in the hard X-ray band by means of a Compton scattering polarimeter on board of each satellite. CUSP will allow to study the magnetic reconnection and particle acceleration in the flaring magnetic structures. CUSP is a project approved for a Phase B study by the Italian Space Agency in the framework of the Alcor program aimed to develop CubeSat technologies and missions. In this paper we describe the a method for a multi-physical simulation analysis while analyzing some possible design optimization of the payload design solutions adopted. In particular, we report the mechanical design for each structural component, the results of static and dynamic finite element analysis, the preliminary thermo-mechanical analysis for two specific thermal cases (hot and cold orbit) and a topological optimization of the interface between the platform and the payload.
format Preprint
id arxiv_https___arxiv_org_abs_2407_04135
institution arXiv
publishDate 2024
record_format arxiv
spellingShingle The multi$-$physics analysis and design of CUSP, a two CubeSat constellation for Space Weather and Solar flares X-ray polarimetry
Lombardi, Giovanni
Fabiani, Sergio
Del Monte, Ettore
Costa, Enrico
Soffitta, Paolo
Muleri, Fabio
Baffo, Ilaria
Biancolini, Marco E.
Bonomo, Sergio
Brienza, Daniele
Campana, Riccardo
Centrone, Mauro
Contini, Gessica
Cucinella, Giovanni
Curatolo, Andrea
De Angelis, Nicolas
De Cesare, Giovanni
Del Re, Andrea
Di Cosimo, Sergio
Di Filippo, Simone
Di Marco, Alessandro
Di Meo, Emanuele
Di Persio, Giuseppe
Donnarumma, Immacolata
Fanelli, Pierluigi
Leonetti, Paolo
Locarini, Alfredo
Loffredo, Pasqualino
Lopez, Andrea
Minervini, Gabriele
Modenini, Dario
Natalucci, Silvia
Negri, Andrea
Perelli, Massimo
Rossi, Monia
Rubini, Alda
Scalise, Emanuele
Terracciano, Andrea
Tortora, Paolo
Zaccagnino, Emanuele
Zambardi, Alessandro
Instrumentation and Methods for Astrophysics
Solar and Stellar Astrophysics
Space Physics
The CUbesat Solar Polarimeter (CUSP) project aims to develop a constellation of two CubeSats orbiting the Earth to measure the linear polarization of solar flares in the hard X-ray band by means of a Compton scattering polarimeter on board of each satellite. CUSP will allow to study the magnetic reconnection and particle acceleration in the flaring magnetic structures. CUSP is a project approved for a Phase B study by the Italian Space Agency in the framework of the Alcor program aimed to develop CubeSat technologies and missions. In this paper we describe the a method for a multi-physical simulation analysis while analyzing some possible design optimization of the payload design solutions adopted. In particular, we report the mechanical design for each structural component, the results of static and dynamic finite element analysis, the preliminary thermo-mechanical analysis for two specific thermal cases (hot and cold orbit) and a topological optimization of the interface between the platform and the payload.
title The multi$-$physics analysis and design of CUSP, a two CubeSat constellation 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/2407.04135