IRIS
SAVINO, RAFFAELE
 Distribuzione geografica
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Continente #
AS - Asia 11.615
NA - Nord America 10.664
EU - Europa 10.295
SA - Sud America 1.212
Continente sconosciuto - Info sul continente non disponibili 557
AF - Africa 223
OC - Oceania 46
Totale 34.612
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Nazione #
US - Stati Uniti d'America 10.033
SG - Singapore 5.306
IT - Italia 3.511
RU - Federazione Russa 2.938
CN - Cina 2.131
VN - Vietnam 1.701
HK - Hong Kong 998
BR - Brasile 936
DE - Germania 737
FR - Francia 569
UA - Ucraina 560
CA - Canada 469
GB - Regno Unito 448
FI - Finlandia 358
IE - Irlanda 307
IN - India 273
JP - Giappone 257
SE - Svezia 241
BD - Bangladesh 229
NL - Olanda 209
KR - Corea 115
ES - Italia 112
AR - Argentina 104
MX - Messico 79
PH - Filippine 70
IQ - Iraq 68
TW - Taiwan 68
TR - Turchia 61
AT - Austria 54
BE - Belgio 52
TH - Thailandia 52
PL - Polonia 50
EC - Ecuador 43
ID - Indonesia 40
PK - Pakistan 40
AU - Australia 36
EG - Egitto 36
CL - Cile 35
ZA - Sudafrica 32
CO - Colombia 26
CI - Costa d'Avorio 25
MA - Marocco 24
IL - Israele 23
PT - Portogallo 22
DZ - Algeria 21
KE - Kenya 19
RO - Romania 19
SA - Arabia Saudita 19
AE - Emirati Arabi Uniti 18
UZ - Uzbekistan 17
VE - Venezuela 17
CR - Costa Rica 16
IR - Iran 16
JO - Giordania 15
PE - Perù 15
BG - Bulgaria 14
BO - Bolivia 13
JM - Giamaica 13
MY - Malesia 13
CH - Svizzera 12
CZ - Repubblica Ceca 12
GR - Grecia 12
LT - Lituania 12
ET - Etiopia 11
KZ - Kazakistan 11
NP - Nepal 11
PY - Paraguay 11
UY - Uruguay 11
LB - Libano 9
TN - Tunisia 9
HN - Honduras 8
GT - Guatemala 7
HU - Ungheria 7
EU - Europa 6
NZ - Nuova Zelanda 6
QA - Qatar 6
BS - Bahamas 5
DO - Repubblica Dominicana 5
EE - Estonia 5
GE - Georgia 5
OM - Oman 5
SY - Repubblica araba siriana 5
TT - Trinidad e Tobago 5
AZ - Azerbaigian 4
BB - Barbados 4
BY - Bielorussia 4
GA - Gabon 4
PA - Panama 4
PS - Palestinian Territory 4
RS - Serbia 4
TJ - Tagikistan 4
AO - Angola 3
KG - Kirghizistan 3
KH - Cambogia 3
LU - Lussemburgo 3
MG - Madagascar 3
MK - Macedonia 3
MN - Mongolia 3
NA - Namibia 3
NG - Nigeria 3
Totale 33.978
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Città #
Singapore 2.516
San Jose 1.322
Hong Kong 934
Chandler 904
Moscow 779
Santa Clara 627
Naples 617
Ashburn 568
Jacksonville 533
Ho Chi Minh City 488
Beijing 420
Hanoi 393
The Dalles 362
Napoli 353
Millbury 316
Lauterbourg 296
Munich 286
Princeton 275
Hefei 258
Los Angeles 234
Montréal 222
Rome 217
Nanjing 209
Boston 181
Buffalo 174
Tokyo 159
Mcallen 142
Wilmington 124
Ottawa 118
Amsterdam 117
New York 116
Dallas 109
Council Bluffs 108
Milan 108
Woodbridge 107
Houston 98
Des Moines 82
São Paulo 79
Redondo Beach 77
Haiphong 76
Kronberg 69
Nanchang 69
Ann Arbor 67
Frankfurt am Main 66
Turin 62
Da Nang 61
Seattle 61
Centro 60
Dublin 60
Hebei 58
Salerno 53
Cagliari 51
Caserta 51
Seoul 50
Boardman 49
Bologna 47
Norwalk 46
Shenyang 44
Chennai 43
Jiaxing 43
Orem 42
Helsinki 41
Lawrence 39
Pune 39
Tianjin 39
Changsha 38
Torre Annunziata 37
Brooklyn 35
Hải Dương 35
Mexico City 35
Vienna 35
Warsaw 35
Atlanta 34
Chicago 34
Madrid 34
San Francisco 34
Lappeenranta 32
London 31
Rio de Janeiro 30
Casoria 29
Santiago 29
Toronto 29
Denver 28
Belo Horizonte 27
Nuremberg 27
Shanghai 27
Taranto 27
Brasília 26
Falkenstein 26
Bangkok 25
Phoenix 25
Kansas City 23
Baghdad 22
Biên Hòa 22
Montreal 21
Mumbai 21
Dong Ket 20
Guangzhou 20
Kunming 20
Can Tho 19
Totale 17.406
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Nome #
Aerothermal Analysis of a Sample-Return Reentry Capsule 869
Mini-IRENE: Design Of Deployable Heat Shield Capsule For A Sounding Rocket Flight Experiment 472
FORCE: A FORmation Flying SAR Based on CubEsat Assemblies 326
Two-Hundred-Newton Laboratory-Scale Hybrid Rocket Testing for Paraffin Fuel-Performance Characterization 283
RODIO Mission Status and Future Developments 274
Development and flight test of a suborbital re-entry demonstrator 250
Experimental and numerical assessment of regression rate and propulsive performance of 10N-class hybrid rockets for nanosatellite maneuvering 239
The Small Mars Satellite: a European small-size Mars lander 238
Ultra-High-Temperature Ceramic Matrix Composites for Hybrid Rocket Nozzles 214
Experimental Characterization of an Impulsive Hydrogen Peroxide-based Rocket for Fine Orbit Control 213
Computational Fluid-dynamic Simulations of Hybrid Rocket Internal Flow Including Discharge Nozzle 208
Aerodynamic study of airframe-engine integration of a supersonic business jet 194
HYBRID ROCKETS WITH NOZZLE IN ULTRA-HIGH-TEMPERATURE CERAMIC COMPOSITES 190
Fast Reconfiguration Maneuvers of a Micro-satellite Constellation Based on a Hybrid Rocket Engine 188
Experimental investigation of N2O decomposition with pd∕al2 o3 cylindrical pellets catalyst 188
Aero-thermo-chemical characterization of ultra-high-temperature ceramics for aerospace applications 180
Hypersonic boost-glide systems: Flight mechanics and plasma parameters evaluation through aero-thermo-chemical computational fluid dynamics 173
Design and testing of a monopropellant thruster based on N2O decomposition in Pd/Al2O3 pellets catalytic bed 165
Experimental characterization of a hydrogen peroxide-based thruster for small satellites 161
Aerodynamic Control System for a Deployable Re-entry Capsule 161
Aerodinamica parte I fondamenti e principi 158
Aerodynamic Control System for a Deployable Re-Entry Capsule 158
DSMC Aero-Thermo-Dynamic Analysis of a Deployable Capsule for Mars Entry 156
Mini Irene Project: Ground Demonstrator Plasma Wind Tunnel Testing 156
A benchmark study on the thermal conductivity of nanofluids 155
Visualization of liquid distribution and dry-out in a single-channel heat pipe with different wettability 153
Effect of SiC concentration on aero-thermal behavior of ZrB2-based ceramics in hypersonic environment 151
Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket 150
Assessment of a deployable aerodynamic control system for microsatellites recovery 149
Combined fluid-dynamic modelling of hybrid rocket internal ballistics and nozzle heat transfer 149
Mixed-Compression Supersonic Intake and Engine–Airframe Integration 146
Thermal performance of self-rewetting fluid heat pipe containing dilute solutions of polymer-capped silver nanoparticles synthesized by microwave-polyol process 145
Aerodynamic Analysis of the Aerospaceplane HYPLANE in Supersonic Rarefied Flow 143
Transient Computational Thermofluid-Dynamic Simulation of Hybrid Rocket Internal Ballistics 142
Effect of hypersonic flow chemical composition on the oxidation behavior of a super-strong UHTC 141
Preliminary design and study of 5N HTP monopropellant thruster for small satellites 140
Design and testing of a paraffin-based hybrid rocket demonstrator 140
Aerodynamic analysis of a flap-based deployable re-entry system in different flight conditions 138
Small Mars satellite: A low-cost system for Mars exploration 138
Computational Fluid-Dynamic Simulations of the Internal Ballistics of Hybrid Rocket Burning Paraffin-based Fuel 138
CHARACTERIZATION OF CARBON-FIBER REINFORCED ULTRA-HIGH-TEMPERATURE CERAMIC MATRIX COMPOSITES IN ARC-JET ENVIRONMENT 138
Non-linear aero-elastic response of a multi-layer TPS 137
Design and Testing of a Paraffin-Based 1000 N HRE Breadboard 135
Propulsion tests on ultra-high-temperature ceramic matrix composites for reusable rocket nozzles 134
Arc-jet wind tunnel characterization of ultra-high-temperature ceramic matrix composites 134
Self-ReWetting capillary flow under evaporation and condensation processes in parabolic flight conditions 132
MODELLING OF PARAFFIN-BASED FUEL COMBUSTION IN HYBRID ROCKETS 132
Capillary rising of self-rewetting solutions in laser engraved micro-channels 131
Aerothermodynamic and feasibility study of a deployable aerobraking re-entry capsule 131
Processing and testing of UHTCMCs for aerospace applications 129
The Small Mars System 129
The application of computational thermo-fluid-dynamics to the simulation of hybrid rocket internal ballistics with classical or liquefying fuels: A review 129
IRENE - Italian re-entry nacelle for microgravity experiments 127
Recent advancements in experimental and numerical characterization of paraffin-based fuels for hybrid rocket application 127
Characterization of novel ceramic composites for rocket nozzles in high-temperature harsh environments 127
Upgrading of an Arc-heated Flow Facility for Reentry Simulation 125
CONVENZIONE NATURALE E ALLA MARANGONI IN SISTEMI LIQUIDI PARZIALMENTE MISCIBILI 124
Regression rate model assessed by ballistic reconstruction technique in hybrid rocket engines burning liquefying fuels 123
Conceptual design of de-orbit and re-entry modules for standard CubeSats 123
Ultra-High-Temperature Testing of Sintered ZrB2-based Ceramic Composites in Atmospheric Re-entry Environment 123
Hybrid Rocket Engines Design for Materials Characterization 122
A new firing test campaign on the 1000 N thrust-class Hyprob hybrid rocket engine 122
Aero-Thermo-Dynamic Analysis of a Low Ballistic Coefficient Deployable Capsule in Earth Re-Entry 122
Rarefied aerodynamics of a deployable re-entry capsule 122
Aerodynamic study of a 3U CubeSat for drag-based in-plane orbital maneuvers in Very Low Earth Orbit 120
Experimental and numerical simulation, by an arc-jet facility, of hypersonic flow in Titan's atmosphere 120
Recent development on heat pipes for ground and space applications 120
Mini-IRENE: The First European Flight Experiment Of A Deployable Heat Shield 120
Planetary entry simulation 119
Self-consistent surface-temperature boundary condition for iquefying-fuel-based hybrid rockets internal-ballistics simulation 119
On a more rational specification for the microgravity environment of the International Space Station 118
Compositionally complex catalytic oxide beds free of noble metals for H2O2 fuelled monopropellant thrusters 117
Regression Rate and Performance Analysis via Ballistic Reconstruction of a small-scale H2O2-based Hybrid Rocket fuelled by Polyvinyl Chloride 117
Adjustable aerobraking heat shield for Satellites deployment and recovery 117
Fast reconfiguration maneuvers of a micro-satellite constellation based on a hybrid rocket engine 116
Studio aerotermodinamico di sistemi di protezione termica innovativi per velivoli ipersonici 115
A study of a high lift wing-body configuration for low earth orbit re-entry. 115
Self rewetting fluids heat transfer experiment selene 115
Testing ultra-high -temperature ceramics for thermal protection and rocket applications 115
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: IAD geometrical effects on the flowfield structure 114
Influenza dell'effetto Marangoni sull'efficienza di heat pipes per applicazioni spaziali 114
Aerothermodynamic and stability analyses of a deployable re-entry capsule 114
Fuel Ignition in HTP Hybrid Rockets at Very Low Mass Fluxes: Challenges and Pulsed Preheating Techniques Using Palladium-Coated Catalysts 113
ESA Project: Innovative Wickless Heat Pipe Systems for Ground and Space Applications 113
Precise Re-Entry and Landing of Propellantless Low Earth Orbit Spacecraft 113
An Improvement of the Gas-surface Interaction and Entrainment Models for Paraffin-based Fuels in Hybrid Rocket Engines 113
Ground-based activities in preparation of microgravity experiments on heat pipes with self-rewetting fluids 112
Innovative heat pipes with self-rewetting fluids under normal and reduced gravity conditions 111
Self-rewetting heat transfer fluids and nano-brines for space heat pipes 111
Aerothermodynamic and system analysis of a small hypersonic airplane (Hyplane) 111
A simplified computational fluid-dynamic approach to the oxidizer injector design in hybrid rockets 111
Effects of solar panels on Aerodynamics of a small satellite with deployable aero-brake 111
Experimental analysis of a Flat Plate Pulsating Heat Pipe with Self-ReWetting Fluids during a parabolic flight campaign 111
Testing and Characterization of Near-Zero-Ablation Fibre-reinforced Ultra High Temperature Ceramics for Aerospace 110
Analisi delle prestazioni di ugelli a spina con gas reagenti 110
Heat pipes with self-rewetting fluids for space applications 110
Heat transfer fluids 110
Numerical aspects of particle-in-cell simulations for plasma-motion modeling of electric thrusters 110
The Importance of an accurate knowledge of the Microgravity environment for potential ISS users 108
Heat transfer characteristics of flat plate pulsating heat pipe using self-rewetting fluids 108
Totale 15.311
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Categoria #
all - tutte 107.966
article - articoli 0
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 107.966
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20221.684 0 22 19 47 27 66 40 82 298 94 242 747
2022/20232.207 353 179 96 235 240 262 37 207 254 115 174 55
2023/20242.027 104 224 112 133 126 172 107 254 66 169 373 187
2024/20258.067 488 663 94 117 379 443 786 568 899 665 2.267 698
2025/202614.185 1.425 994 1.245 1.147 2.160 619 1.516 1.136 2.084 889 449 521
2026/2027714 555 159 0 0 0 0 0 0 0 0 0 0
Totale 34.612