The mass optimization of payloads for space applications is always one of the main drivers in the design phase. This paper presents the evolution of the design from the breadboard of the DORA telescope, through a structural redesign in order to achieve competitive overall performance with minimum mass. A generative optimization technique has been applied to allow an effective distribution of the mass in the component. The optimized component has been manufactured and verification tests performed to validate the developed model.

Structural optimization of supporting structures for the DORA telescope

Valnegri P.;Scaccabarozzi D.;Saggin B.
2023-01-01

Abstract

The mass optimization of payloads for space applications is always one of the main drivers in the design phase. This paper presents the evolution of the design from the breadboard of the DORA telescope, through a structural redesign in order to achieve competitive overall performance with minimum mass. A generative optimization technique has been applied to allow an effective distribution of the mass in the component. The optimized component has been manufactured and verification tests performed to validate the developed model.
2023
2023 IEEE 10th International Workshop on Metrology for AeroSpace, MetroAeroSpace 2023 - Proceedings
978-1-6654-5690-6
Deployable space telescope
deployment mechanism
DORA project
generative design
mechanical design
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/1254031
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