| Design and development of a LOX/LCH4 technology demonstrator V Salvatore, F Battista, R Votta, M Di Clemente, M Ferraiuolo, P Roncioni, ... 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 3935, 2012 | 30 | 2012 |
| Combustion instability and pressure oscillation numerical simulation in a solid rocket motor AD French, M Panelli, G Di Lorenzo, A Schettino, F Paglia 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 4952, 2017 | 20 | 2017 |
| Development of a LOX/LCH4 Technology Demonstrator Based on Regenerative Cooling throughout Validation of Critical Design Aspects with Breadboards in the Framework of the Hyprob … F Battista, M Di Clemente, M Ferraiuolo, R Votta, D Ricci, M Panelli, ... 63rd International Astronautical Congress, Naples, Italy. IAC-2012, 2012 | 16 | 2012 |
| Thermal fluid dynamics analysis of vented brake disc rotor with ribs turbulators M Panelli, G Cardone Thermal and Environmental Issues in Energy Systems, ASME-UIT-ATI …, 2010 | 13 | 2010 |
| Axisymmetric hybrid plasma model for Hall effect thrusters M Panelli, D Morfei, B Milo, FA D’Aniello, F Battista Particles 4 (2), 296-324, 2021 | 12 | 2021 |
| CFD modelling and simulations of the HYPROB regenerative LOX/CH4 thrust chamber P Roncioni, D Cardillo, M Panelli, D Ricci, M Di Clemente, F Battista 5th European Conference For Aeronautics And Space Sciences (EUCASS), 2013 | 11 | 2013 |
| Heat transfer enhancement of natural convection with ribs M Imbriale, M Panelli, G Cardone Quantitative InfraRed Thermography Journal 9 (1), 55-67, 2012 | 10 | 2012 |
| An improved approach for hybrid rocket injection system design M Invigorito, G Elia, M Panelli International Journal of Aerospace and Mechanical Engineering 10 (4), 686-696, 2016 | 8 | 2016 |
| LOX/GCH4 Heat Sink Combustion Chamber: Testing and Preliminary Assessment of Experimental Data F Battista, D Cardillo, P Natale, M Panelli, M Fragiacomo Space Propulsion Conference 2016, 2016 | 6 | 2016 |
| The HYPROB Liquid Rocket Engine Demonstrator: CFD Modeling and Simulations M Panelli, D Cardillo, D Ricci, P Roncioni, F Battista 4th Space Propulsion Conference, 19-22, 2014 | 6 | 2014 |
| NUMERICAL SIMULATION OF A LO2-CH4 ROCKET ENGINE DEMONSTRATOR D Cardillo, BF Panelli, Mario,Ricci Daniele, Roncioni Pietro 65th International Astronautical Congress, 2014 | 6 | 2014 |
| A plasma model for orificed hollow cathode M Panelli, C Giaquinto, A Smoraldi, F Battista Proceedings of the 36th International Electric Propulsion Conference …, 2019 | 5 | 2019 |
| Numerical Modeling of Self-Pressurizing Oxidizers for Hybrid Rocket Injection M Invigorito, G Elia, M Panelli 6th European Conference for Aeronautics and Space Sciences, 2015 | 5 | 2015 |
| Numerical prediction of nozzle ablation in hybrid rocket engine M Panelli, D Cardillo, M Di Clemente, G Ranuzzi 6th EUCASS 29, 2015 | 5 | 2015 |
| Development of a cathode for low-power Hall Effect Thruster M Panelli, FB Battista, A Smoraldi, M Fragiacomo AIAA Propulsion and Energy 2021 Forum, 3387, 2021 | 3 | 2021 |
| A Preliminary Design Tool for Hollow Cathodes M Panelli, A Smoraldi, F Battista 35th International Electric Propulsion Conference, IEPC2017, Georgia …, 2017 | 3 | 2017 |
| Scaling of Magnetic Circuit for Magnetically Shielded Hall Effect Thrusters E Lopedote, M Panelli, F Battista Aerotecnica Missili & Spazio 102 (2), 109-125, 2023 | 2 | 2023 |
| Preliminary design of helicon plasma thruster by means of particle swarm optimization G Coppola, M Panelli, F Battista AIP Advances 13 (5), 2023 | 2 | 2023 |
| Particle-in-cell simulation of heavy species in Hall effect discharge A Petronelli, M Panelli, F Battista Aerotecnica Missili & Spazio 101 (2), 143-157, 2022 | 2 | 2022 |
| Fluid Simulation of Electron Discharge in Hall Effect Thruster M Panelli, F Battista Italian Association of Aeronautics and Astronautics (AIDAA) XXVI …, 2021 | 2 | 2021 |
Francesco BattistaCIRA, italian aerospace research centerEmail verificata su cira.it
