polito.it

Login

Webthesis
Libraries

Thesis by Mastrovito, Domenico

Group by: Item Type | No Grouping

Number of items: 1.

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 May 28 14:14:05 2024 CEST.

Contacts