Heat transfer modeling for supercritical methane flowing in rocket engine cooling channels M Pizzarelli, F Nasuti, M Onofri, P Roncioni, R Votta, F Battista Applied Thermal Engineering 75, 600-607, 2015 | 67 | 2015 |
Experimental investigation of transcritical methane flow in rocket engine cooling channel R Votta, F Battista, V Salvatore, M Pizzarelli, G Leccese, F Nasuti, S Meyer Applied Thermal Engineering 101, 61-70, 2016 | 47 | 2016 |
Two-hundred-newton laboratory-scale hybrid rocket testing for paraffin fuel-performance characterization GD Di Martino, S Mungiguerra, C Carmicino, R Savino, D Cardillo, ... Journal of Propulsion and Power 35 (1), 224-235, 2019 | 37 | 2019 |
Experimental and numerical investigation on the behaviour of methane in supercritical conditions D Ricci, P Natale, F Battista Applied Thermal Engineering 107, 1334-1353, 2016 | 35 | 2016 |
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 |
Validation of conjugate heat transfer model for rocket cooling with supercritical methane M Pizzarelli, F Nasuti, R Votta, F Battista Journal of Propulsion and Power 32 (3), 726-733, 2016 | 25 | 2016 |
Hypersonic aerothermal environment preliminary definition of the cira ftb-x reentry vehicle G Pezzella, F Battista, A Schettino, M Marini, P De Matteis Proceedings of the west-east high speed flow field conference, 19-22, 2007 | 25 | 2007 |
A review of the Hall thruster scaling methodology F Battista, EA De Marco, T Misuri, M Andrenucci Proc. 30th International Electric Propulsion Conference (IEPC 07). IEPC-2007-313, 2007 | 25 | 2007 |
High power Hall thruster design options T Misuri, F Battista, C Barbieri, EA De Marco, M Andrenucci Proceedings of the 30th International Electric Propulsion Conference …, 2007 | 24 | 2007 |
Hall thruster scaling methodology M Andrenucci, F Battista, P Piliero The 29th Int. Electric Prop. Conf., Princeton University, 31 October–4 …, 2005 | 24 | 2005 |
Design and testing of a paraffin-based 1000 N HRE breadboard F Battista, D Cardillo, M Fragiacomo, GD Di Martino, S Mungiguerra, ... Aerospace 6 (8), 89, 2019 | 18 | 2019 |
Particles in turbulent separated flow over a bump: Effect of the Stokes number and lift force JP Mollicone, M Sharifi, F Battista, P Gualtieri, CM Casciola Physics of Fluids 31 (10), 2019 | 16 | 2019 |
Single-injector LOX/GCH4 combustion chambers manufacturing and experimental characterization in the framework of the HYPROB-BREAD project F Battista, M Ferraiuolo, P Natale, D Cardillo, A French, D Ricci, ... Space Propulsion Conference, 2014 | 16 | 2014 |
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 |
Experimental investigations on the magneto-hydro-dynamic interaction around a blunt body in a hypersonic unseeded air flow A Cristofolini, CA Borghi, G Neretti, A Schettino, E Trifoni, F Battista, ... Journal of Applied Physics 112 (9), 2012 | 15 | 2012 |
Transcritical behavior of methane in the cooling jacket of a liquid-oxygen/liquid-methane rocket-engine demonstrator D Ricci, F Battista, M Fragiacomo Energies 15 (12), 4190, 2022 | 14 | 2022 |
Cooling channel analysis of a LOX/LCH4 rocket engine demonstrator M Pizzarelli, B Betti, F Nasuti, D Ricci, P Roncioni, F Battista, V Salvatore 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 4004, 2014 | 14 | 2014 |
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 | 13 | 2021 |
Modelling, Testing and Design Considerations of a GOX/GCH4 Igniter for a HYPROB-SSBB Single Injector Thrust Chamber F Battista, M Ferraiuolo, A Martucci, M Fragiacomo, P Natale, D Ricci, ... Journal of the British Interplanetary Society 1 (2014), 67, 2014 | 13 | 2014 |
Recent progress on the development of a LOX/LCH4 rocket engine demonstrator in the framework of the Italian HYPROB program V Salvatore, F Battista, P De Matteis, M Rudnykh, L Arione, F Ceccarelli 64rd International Astronautical Congress, IAC-13 C 4, 3, 2013 | 13 | 2013 |