Sfoglia per Autore
CONCEPTUAL DESIGN OF THE ELECTRIC PUMPS FOR THE HIGH-PERFORMANCE ENGINE OF A EUROPEAN LUNAR LANDER
2023 Danieli, P.; Masi, M.; Tridello, R.; Pessana, M.; Barato, F.; Chiesa, A.
Modeling and CFD Simulation of Regression Rate in Hybrid Rocket Motors
2023 Rampazzo, A.; Barato, F.
Review of Alternative Sustainable Fuels for Hybrid Rocket Propulsion
2023 Barato, F.
Optimal use of electric propulsion for drag compensation in very low earth orbit on satellites with deployable solar panels
2023 Barato, F.
A Simplified Thermal Analysis Model for Regeneratively Cooled Rocket Engine Thrust Chambers and Its Calibration with Experimental Data
2023 Fagherazzi, M.; Santi, M.; Barato, F.; Pizzarelli, M.
Design and In-orbit Demonstration of REGULUS, an Iodine electric propulsion system
2022 Bellomo, N.; Magarotto, M.; Manente, M.; Trezzolani, F.; Mantellato, R.; Cappellini, L.; Paulon, D.; Selmo, A.; Scalzi, D.; Minute, M.; Duzzi, M.; Barbato, A.; Schiavon, A.; Di Fede, S.; Souhair, N.; De Carlo, P.; Barato, F.; Milza, F.; Toson, E.; Pavarin, D.
Comparison between Different Re-Entry Technologies for Debris Mitigation in LEO
2022 Barato, F.
Real-Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor
2022 Ruffin, Alessandro; Paccagnella, Enrico; Santi, Marco; Barato, Francesco; Pavarin, Daniele
OPTIMAL USE OF ELECTRIC PROPULSION FOR DRAG COMPENSATION IN VERY LOW EARTH ORBIT ON SATELLITES WITH DEPLOYABLE SOLAR PANELS
2021 Barato, Francesco
Challenges of ablatively cooled hybrid rockets for satellites or upper stages
2021 Barato, F.
REGULUS: INTEGRATION AND TESTING OF AN IODINE ELECTRIC PROPULSION SYSTEM
2021 Bellomo, Nicolas; Magarotto, Mirko; Manente, Marco; Trezzolani, Fabio; Mantellato, Riccardo; Cappellini, Lorenzo; Paulon, Devis; Selmo, ANTONIO FRANCO; Scalzi, Davide; Minute, Marco; Duzzi, Matteo; Barbato, Alessandro; Schiavon, Alessandro; Souhair, Nabil; DI FEDE, Simone; DE CARLO, Paola; Barato, Francesco; Toson, Elena; Pavarin, Daniele
Design and Testing of a 3D Printed Regenerative Cooled Nozzle for a Hydrogen Peroxide based Bi-Propellant Thruster
2021 Fagherazzi, Matteo; Santi, Marco; Barato, Francesco; Pavarin, Daniele
Correction to: Design and Testing of a 3D Printed Regenerative Cooled Nozzle for a Hydrogen Peroxide based Bi-Propellant Thruster (AIAA Propulsion and Energy Forum, 2021)
2021 Fagherazzi, Matteo; Santi, Marco; Barato, Francesco; Pavarin, Daniele
Development of the Propulsion System for a Moon Drone Vehicle Demonstrator
2021 Ruffin, Alessandro; Fagherazzi, Matteo; Bellomo, Nicolas; Barato, Francesco; Pavarin, Daniele; Pessana, Mario
Variations and Control of Thrust and Mixture Ratio in Hybrid Rocket Motors
2021 Barato, Francesco; Toson, Elena; Pavarin, Daniele
Variations and Control of Thrust and Mixture Ratio in Hybrid Rocket Motors
2020 Barato, Francesco; Toson, Elena; Pavarin, Daniele
Design and testing of a hydrogen peroxide bipropellant thruster
2020 Santi, Marco; Fagherazzi, Matteo; Barato, Francesco; Pavarin, Daniele
Impact of propulsion system characteristics on the potential for cost reduction of earth observation missions at very low altitudes
2020 Bertolucci, G.; Barato, F.; Toson, E.; Pavarin, D.
Numerical analyses of thermal protection design in hybrid rocket motors
2020 Barato, F.; Paccagnella, E.; Franco, M.; Pavarin, D.
Explicit analytical equations for single port hybrid rocket combustion chamber sizing
2020 Barato, F.; Paccagnella, E.; Pavarin, D.
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