Följ
Francesco Battista
Francesco Battista
CIRA, italian aerospace research center
Verifierad e-postadress på cira.it - Startsida
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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
722015
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
482016
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
392019
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
382016
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
332012
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
272016
Hypersonic aerothermal environment preliminary definition of the cira ftb-x reentry vehicle
G Pezzella, F Battista, A Schettino, M Marini, P De Matteis
Environment, 1-25, 2007
262007
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
262007
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
242007
Hall thruster scaling methodology
M Andrenucci, F Battista, P Piliero
The 29th Int. Electric Prop. Conf., Princeton University, 31 October–4 …, 2005
242005
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
192019
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
162019
Single-injector LOX/GCH4 combustion chambers manufacturing and experimental characterization in the framework of HYPROB-BREAD project
F Battista, M Ferraiuolo, P Natale, D Cardillo, A French, D Ricci, ...
Space Propulsion Conference, 2014
162014
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
162012
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
152022
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
152014
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
152012
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
142021
Oxygen–methane rocket thrust chambers: Review of heat transfer experimental studies
M Pizzarelli, F Battista
Acta Astronautica 209, 48-66, 2023
132023
Thermo-structural and thermo-fluid dynamics analyses supporting the design of the cooling system of a methane liquid rocket engine
M Ferraiuolo, D Ricci, F Battista, P Roncioni, V Salvatore
ASME International Mechanical Engineering Congress and Exposition 46421 …, 2014
132014
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Artiklar 1–20