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Thesis by Mastrovito, Domenico

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Thesis

Domenico Mastrovito. Ascent Trajectory Optimization for a Hybrid Propulsion Mini Launcher. Rel. Dario Giuseppe Pastrone. Politecnico di Torino, Corso di laurea magistrale in Ingegneria Aerospaziale, 2020

This list was generated on Tue Aug 9 22:26:10 2022 CEST.