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Raffaele Savino

Full Professor

Università di Napoli Federico II

Napoli, Italia

Hypersonics, Space Technologies, Microgravity, Space Propulsion, Fluid dynamics

Fluid Dynamics, UNIVERSITA DEGLI STUDI DI NAPOLI FEDERICO II. Italia, 1993

Full Professor Full Time

UNIVERSITA DEGLI STUDI DI NAPOLI FEDERICO II

Engineering

Napoli, Italia

2016 - A la fecha

Raffaele Savino

STANFORD UNIVERSITY

Estados Unidos, 2020

2020-2022 top 2 per cent of the most-cited scientists according to the Stanford University ranking


New Entrainment Model for Modelling the Regression Rate in Hybrid Rocket Engines Gallo, Giuseppe; Mungiguerra, S.; Savino, Raffaele Article JOURNAL OF PROPULSION AND POWER (2021)
Numerical aspects of particle-in-cell simulations for plasma-motion modeling of electric thrusters Gallo, G.; Isoldi, A.; Del Gatto, D.; Savino, R.; Capozzoli, A.; Curcio, C.; Liseno, A. Article AEROSPACE SERIES (2021)
Precise re-entry and landing of propellantless spacecraft Fedele, Alberto; Omar, Sanny; Cantoni, Stefania; Savino, Raffaele; Bevilacqua, Riccardo Article ADVANCES IN SPACE RESEARCH-SERIES (2021)
Qualification and reusability of long and short fibre-reinforced ultra-refractory composites for aerospace thermal protection systems Mungiguerra, S.; Silvestroni, L.; Savino, R.; Zoli, L.; Esser, B.; Lagos, M.; Sciti, D. Article Corrosion Science (2021)
S4 - A demonstrator of HYPLANE, a single stage suborbital spaceplane and a hypersonic business jet Russo, Gennaro; Voto, Claudio; Savino, Raffaele Article ACTA ASTRONAUTICA (2021)
Self-consistent surface-temperature boundary condition for iquefying-fuel-based hybrid rockets internal-ballistics simulation Carmicino, C.; Gallo, G.; Savino, R. Article International Journal of Heat and Mass Transfer (2021)
Aerodynamic Control System for a Deployable Re-entry Capsule Article ACTA ASTRONAUTICA (2020)
Characterization of novel ceramic composites for rocket nozzles in high-temperature harsh environments Mungiguerra, S.; Di Martino, G. D.; Savino, R.; Zoli, L.; Silvestroni, L.; Sciti, D. Article International Journal of Heat and Mass Transfer (2020)
Design and testing of a monopropellant thruster based on N2O decomposition in Pd/Al2O3 pellets catalytic bed Di Martino, G. D.; Gallo, G.; Mungiguerra, S.; Festa, G.; Savino, R Article ACTA ASTRONAUTICA (2020)
Experimental investigation of N2O decomposition with pd∕al2 o3 cylindrical pellets catalyst Gallo, G.; Di Martino, G. D.; Festa, G.; Savino, R. Article JOURNAL OF SPACECRAFT AND ROCKETS (2020)
Improved aero-thermal resistance capabilities of ZrB2-based ceramics in hypersonic environment for increasing SiC content Mungiguerra, Stefano; Cecere, Anselmo; Savino, Raffaele; Saraga, Federico; Monteverde, Frédéric; Sciti, Diletta Article Corrosion Science (2020)
Ultra-High-Temperature Testing of Sintered ZrB2-based Ceramic Composites in Atmospheric Re-entry Environment Mungiguerra, S.; Di Martino, G. D.; Cecere, A.; Savino, R.; Zoli, L.; Silvestroni, L.; Sciti, D. Article International Journal of Heat and Mass Transfer (2020)
Aerothermodynamic analyses and redesign of GHIBLI Plasma Wind Tunnel hypersonic diffuser Agostinelli , Pasquale; Trifoni, Eduardo; Savino, Raffaele Article AEROSPACE SCIENCE AND TECHNOLOGY (2019)
Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket Di Martino G.D.; Mungiguerra, S.; Carmicino, C.; Savino, R. Article AEROSPACE SCIENCE AND TECHNOLOGY (2019)
Design and Testing of a Paraffin-Based 1000 N HRE Breadboard Battista, Francesco; Cardillo, Daniele; Fragiacomo, Manrico; Di Martino, Giuseppe Daniele; Mungiguerra, Stefano; Savino, Raffaele Article AEROSPACE SERIES (2019)
Effect of hypersonic flow chemical composition on the oxidation behavior of a super-strong UHTC Silvestroni, L.; Mungiguerra, Stefano; Sciti, D.; Di Martico, Giuseppe D.; Savino, R. Article Corrosion Science (2019)
Research on Heat Transfer Performance of the Open-Loop Micro Pulsating Heat Pipe with Self-Rewetting Fluids Fumoto, K.; Sasa, M.; Okabe, T.; Savino, R.; Inamura, T.; Shirota, M. Article MICROGRAVITY, SCIENCE AND TECHNOLOGY (2019)
The application of computational thermo-fluid-dynamics to the simulation of hybrid rocket internal ballistics with classical or liquefying fuels: A review Di Martino, G. D.; Carmicino, Carmine; Mungiguerra, Stefano.; Savino, R. Article AEROSPACE (2019)
Thermal stability under laser heating of hot-pressed (Hf1-X ZrX)B2/SiC powder mixtures obtained by mechano-synthesis Monteverde, F.; Cordoba, J. M.; Savino, R.; Cecere, A.; Genna, S.; Leone, C. Article JOURNAL OF THE EUROPEAN CERAMIC SOCIETY (2019)
Arc-jet wind tunnel characterization of ultra-high-temperature ceramic matrix composites Mungiguerra, S.; Di Martino, G. D.; Cecere, A.; Savino, R.; Silvestroni, L.; Vinci, A.; Zoli, L.; Sciti, D. Article Corrosion Science (2018)
Effects of solar panels on Aerodynamics of a small satellite with deployable aero-brake Mungiguerra, S.; Zuppardi, G.; Spanò Cuomo, L.; Savino, R. Article ACTA ASTRONAUTICA (2018)
Experimental analysis of a Flat Plate Pulsating Heat Pipe with Self-ReWetting Fluids during a parabolic flight campaign Cecere, Anselmo; De Cristofaro, Davide; Savino, Raffaele; Ayel, Vincent; Sole-Agostinelli, Thibaud; Marengo, Marco; Romestant, Cyril; Bertin, Yves Article ACTA ASTRONAUTICA (2018)
Testing ultra-high -temperature ceramics for thermal protection and rocket applications Savino, Raffaele; Mungiguerra, Stefano; Di Martino, Giuseppe D. Article ADVANCES IN APPLIED CERAMICS (2018)
Two-Hundred-Newton Laboratory-Scale Hybrid Rocket Testing for Paraffin Fuel-Performance Characterization Di Martino, G. D.; Mungiguerra, S.; Carmicino, C.; Savino, R.; Cardillo, D.; Battista, F.; Invigorito, M.; Elia, G. Article JOURNAL OF PROPULSION AND POWER (2018)
Visualization of liquid distribution and dry-out in a single-channel heat pipe with different wettability Cecere, Anselmo; De Cristofaro, Davide; Savino, Raffaele; Boveri, G; Raimondo, Mr; Veronesi, F; Oukara, F; Rioboo, R Article EXPERIMENTAL THERMAL AND FLUID SCIENCE (2018)


Computational Fluid-Dynamic Simulations of the Internal Ballistics of Hybrid Rocket Burning Paraffin-based Fuel Di Martino, G. D.; Mungiguerra, S.; Carmicino, C.; Savino, R. ConferencePaper (2018)

Raffaele Savino

Full Professor

Industrial Engineering

Università di Napoli Federico II

Napoli, Italia

Raffaele Savino

Líneas de Investigación

Educación

Fluid Dynamics, UNIVERSITA DEGLI STUDI DI NAPOLI FEDERICO II. Italia, 1993

Experiencia Académica

Full Professor Full Time

Premios y Distinciones

Raffaele Savino

Article (25)

New Entrainment Model for Modelling the Regression Rate in Hybrid Rocket Engines

Numerical aspects of particle-in-cell simulations for plasma-motion modeling of electric thrusters

Precise re-entry and landing of propellantless spacecraft

Qualification and reusability of long and short fibre-reinforced ultra-refractory composites for aerospace thermal protection systems

S4 - A demonstrator of HYPLANE, a single stage suborbital spaceplane and a hypersonic business jet

Self-consistent surface-temperature boundary condition for iquefying-fuel-based hybrid rockets internal-ballistics simulation

Aerodynamic Control System for a Deployable Re-entry Capsule

Characterization of novel ceramic composites for rocket nozzles in high-temperature harsh environments

Design and testing of a monopropellant thruster based on N2O decomposition in Pd/Al2O3 pellets catalytic bed

Experimental investigation of N2O decomposition with pd∕al2 o3 cylindrical pellets catalyst

Improved aero-thermal resistance capabilities of ZrB2-based ceramics in hypersonic environment for increasing SiC content

Ultra-High-Temperature Testing of Sintered ZrB2-based Ceramic Composites in Atmospheric Re-entry Environment

Aerothermodynamic analyses and redesign of GHIBLI Plasma Wind Tunnel hypersonic diffuser

Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket

Design and Testing of a Paraffin-Based 1000 N HRE Breadboard

Effect of hypersonic flow chemical composition on the oxidation behavior of a super-strong UHTC

Research on Heat Transfer Performance of the Open-Loop Micro Pulsating Heat Pipe with Self-Rewetting Fluids

The application of computational thermo-fluid-dynamics to the simulation of hybrid rocket internal ballistics with classical or liquefying fuels: A review

Thermal stability under laser heating of hot-pressed (Hf1-X ZrX)B2/SiC powder mixtures obtained by mechano-synthesis

Arc-jet wind tunnel characterization of ultra-high-temperature ceramic matrix composites

Effects of solar panels on Aerodynamics of a small satellite with deployable aero-brake

Experimental analysis of a Flat Plate Pulsating Heat Pipe with Self-ReWetting Fluids during a parabolic flight campaign

Testing ultra-high -temperature ceramics for thermal protection and rocket applications

Two-Hundred-Newton Laboratory-Scale Hybrid Rocket Testing for Paraffin Fuel-Performance Characterization

Visualization of liquid distribution and dry-out in a single-channel heat pipe with different wettability

ConferencePaper (1)

Computational Fluid-Dynamic Simulations of the Internal Ballistics of Hybrid Rocket Burning Paraffin-based Fuel

Raffaele Savino