This paper will illustrate the simulations and analysis performed to design the VIPER mission, in preparation for an experimental campaign, carried out within the context of the REXUS/BEXUS programme, on board REXUS-36 in March 2026. The planned experimental activities aim at addressing the data gap in literature regarding the dynamic characterization of small launch vehicles. This is achieved through the analysis of response data recorded during sub-orbital flight. with the final goal of advancing predictive models for design and testing.

Simulations and Experiment Design for the REXUS-36 VIPER Mission / Antonini, Daniele; Pantalani, Tommaso; Chiavari, Lorenzo; Galassi, Luca; Onofri, Ludovica; Piergentili, Fabrizio; Coppotelli, Giuliano. - (2025), pp. 5462-5475. (Intervento presentato al convegno European Conference for AeroSpace Sciences (EUCASS) tenutosi a Rome, Italy).

Simulations and Experiment Design for the REXUS-36 VIPER Mission

Daniele Antonini;Tommaso Pantalani;Luca Galassi;Ludovica Onofri;Fabrizio Piergentili;Giuliano Coppotelli
2025

Abstract

This paper will illustrate the simulations and analysis performed to design the VIPER mission, in preparation for an experimental campaign, carried out within the context of the REXUS/BEXUS programme, on board REXUS-36 in March 2026. The planned experimental activities aim at addressing the data gap in literature regarding the dynamic characterization of small launch vehicles. This is achieved through the analysis of response data recorded during sub-orbital flight. with the final goal of advancing predictive models for design and testing.
2025
European Conference for AeroSpace Sciences (EUCASS)
operational modal analysis; optimal sensor placement; sensor insulation
04 Pubblicazione in atti di convegno::04b Atto di convegno in volume
Simulations and Experiment Design for the REXUS-36 VIPER Mission / Antonini, Daniele; Pantalani, Tommaso; Chiavari, Lorenzo; Galassi, Luca; Onofri, Ludovica; Piergentili, Fabrizio; Coppotelli, Giuliano. - (2025), pp. 5462-5475. (Intervento presentato al convegno European Conference for AeroSpace Sciences (EUCASS) tenutosi a Rome, Italy).
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/1749737
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