IRIS
SAVINO, RAFFAELE
 Distribuzione geografica
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Continente #
AS - Asia 11.428
EU - Europa 10.101
NA - Nord America 9.948
SA - Sud America 1.186
AF - Africa 220
OC - Oceania 46
Continente sconosciuto - Info sul continente non disponibili 11
Totale 32.940
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Nazione #
US - Stati Uniti d'America 9.369
SG - Singapore 5.300
IT - Italia 3.354
RU - Federazione Russa 2.938
CN - Cina 2.102
VN - Vietnam 1.692
HK - Hong Kong 994
BR - Brasile 922
DE - Germania 733
FR - Francia 561
UA - Ucraina 560
CA - Canada 447
GB - Regno Unito 442
FI - Finlandia 358
IE - Irlanda 305
IN - India 263
JP - Giappone 254
SE - Svezia 241
NL - Olanda 204
BD - Bangladesh 115
KR - Corea 113
ES - Italia 110
AR - Argentina 100
MX - Messico 78
IQ - Iraq 68
PH - Filippine 68
TW - Taiwan 68
TR - Turchia 61
AT - Austria 53
TH - Thailandia 52
BE - Belgio 50
PL - Polonia 49
EC - Ecuador 41
PK - Pakistan 40
ID - Indonesia 38
AU - Australia 36
EG - Egitto 36
CL - Cile 35
ZA - Sudafrica 32
CI - Costa d'Avorio 25
CO - Colombia 24
MA - Marocco 24
IL - Israele 23
PT - Portogallo 22
DZ - Algeria 21
KE - Kenya 19
AE - Emirati Arabi Uniti 18
RO - Romania 18
SA - Arabia Saudita 18
UZ - Uzbekistan 17
IR - Iran 15
JO - Giordania 15
VE - Venezuela 15
BG - Bulgaria 13
BO - Bolivia 13
PE - Perù 13
CH - Svizzera 12
CZ - Repubblica Ceca 12
LT - Lituania 12
MY - Malesia 12
ET - Etiopia 11
GR - Grecia 11
KZ - Kazakistan 11
PY - Paraguay 11
UY - Uruguay 11
CR - Costa Rica 9
LB - Libano 9
NP - Nepal 9
TN - Tunisia 8
HN - Honduras 7
HU - Ungheria 7
JM - Giamaica 7
EU - Europa 6
NZ - Nuova Zelanda 6
QA - Qatar 6
DO - Repubblica Dominicana 5
EE - Estonia 5
GE - Georgia 5
OM - Oman 5
SY - Repubblica araba siriana 5
AZ - Azerbaigian 4
GA - Gabon 4
PS - Palestinian Territory 4
RS - Serbia 4
TJ - Tagikistan 4
TT - Trinidad e Tobago 4
AO - Angola 3
BB - Barbados 3
BS - Bahamas 3
BY - Bielorussia 3
KG - Kirghizistan 3
KH - Cambogia 3
MG - Madagascar 3
MK - Macedonia 3
MN - Mongolia 3
NA - Namibia 3
NG - Nigeria 3
NO - Norvegia 3
PA - Panama 3
SI - Slovenia 3
Totale 32.863
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Città #
Singapore 2.512
San Jose 1.268
Hong Kong 931
Chandler 904
Moscow 779
Santa Clara 602
Naples 593
Jacksonville 531
Ashburn 497
Ho Chi Minh City 486
Beijing 419
Hanoi 388
The Dalles 362
Napoli 353
Millbury 316
Lauterbourg 296
Munich 286
Princeton 275
Hefei 258
Montréal 222
Los Angeles 209
Nanjing 209
Rome 186
Boston 179
Buffalo 163
Tokyo 158
Mcallen 142
Wilmington 123
Ottawa 118
Amsterdam 117
Woodbridge 106
New York 105
Dallas 100
Houston 96
Milan 95
Des Moines 81
Redondo Beach 77
Haiphong 75
São Paulo 72
Kronberg 69
Nanchang 69
Ann Arbor 67
Frankfurt am Main 66
Da Nang 61
Centro 60
Dublin 60
Seattle 60
Turin 59
Hebei 58
Salerno 53
Cagliari 51
Caserta 51
Boardman 49
Seoul 49
Bologna 46
Norwalk 46
Council Bluffs 44
Shenyang 44
Jiaxing 43
Chennai 42
Orem 42
Helsinki 41
Lawrence 39
Pune 39
Tianjin 39
Changsha 37
Torre Annunziata 37
Hải Dương 35
Mexico City 35
Vienna 35
Warsaw 35
San Francisco 34
Madrid 33
Lappeenranta 32
London 30
Rio de Janeiro 30
Atlanta 29
Brooklyn 29
Santiago 29
Casoria 28
Belo Horizonte 27
Chicago 27
Shanghai 27
Taranto 27
Falkenstein 26
Nuremberg 26
Bangkok 25
Brasília 25
Denver 24
Phoenix 23
Toronto 23
Baghdad 22
Biên Hòa 22
Kansas City 22
Montreal 21
Dong Ket 20
Guangzhou 20
Kunming 20
Can Tho 19
Mumbai 19
Totale 16.989
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Nome #
Aerothermal Analysis of a Sample-Return Reentry Capsule 867
Mini-IRENE: Design Of Deployable Heat Shield Capsule For A Sounding Rocket Flight Experiment 464
FORCE: A FORmation Flying SAR Based on CubEsat Assemblies 295
Two-Hundred-Newton Laboratory-Scale Hybrid Rocket Testing for Paraffin Fuel-Performance Characterization 281
Development and flight test of a suborbital re-entry demonstrator 239
The Small Mars Satellite: a European small-size Mars lander 238
Experimental and numerical assessment of regression rate and propulsive performance of 10N-class hybrid rockets for nanosatellite maneuvering 231
Ultra-High-Temperature Ceramic Matrix Composites for Hybrid Rocket Nozzles 211
Experimental Characterization of an Impulsive Hydrogen Peroxide-based Rocket for Fine Orbit Control 208
Computational Fluid-dynamic Simulations of Hybrid Rocket Internal Flow Including Discharge Nozzle 205
Aerodynamic study of airframe-engine integration of a supersonic business jet 192
RODIO Mission Status and Future Developments 191
HYBRID ROCKETS WITH NOZZLE IN ULTRA-HIGH-TEMPERATURE CERAMIC COMPOSITES 186
Aero-thermo-chemical characterization of ultra-high-temperature ceramics for aerospace applications 179
Hypersonic boost-glide systems: Flight mechanics and plasma parameters evaluation through aero-thermo-chemical computational fluid dynamics 162
Design and testing of a monopropellant thruster based on N2O decomposition in Pd/Al2O3 pellets catalytic bed 162
Experimental characterization of a hydrogen peroxide-based thruster for small satellites 157
Aerodynamic Control System for a Deployable Re-Entry Capsule 157
Aerodynamic Control System for a Deployable Re-entry Capsule 157
Mini Irene Project: Ground Demonstrator Plasma Wind Tunnel Testing 154
DSMC Aero-Thermo-Dynamic Analysis of a Deployable Capsule for Mars Entry 153
A benchmark study on the thermal conductivity of nanofluids 152
Aerodinamica parte I fondamenti e principi 151
Visualization of liquid distribution and dry-out in a single-channel heat pipe with different wettability 149
Assessment of a deployable aerodynamic control system for microsatellites recovery 147
Combined fluid-dynamic modelling of hybrid rocket internal ballistics and nozzle heat transfer 146
Mixed-Compression Supersonic Intake and Engine–Airframe Integration 143
Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket 143
Thermal performance of self-rewetting fluid heat pipe containing dilute solutions of polymer-capped silver nanoparticles synthesized by microwave-polyol process 140
Transient Computational Thermofluid-Dynamic Simulation of Hybrid Rocket Internal Ballistics 140
Aerodynamic Analysis of the Aerospaceplane HYPLANE in Supersonic Rarefied Flow 139
Small Mars satellite: A low-cost system for Mars exploration 138
Effect of hypersonic flow chemical composition on the oxidation behavior of a super-strong UHTC 138
Non-linear aero-elastic response of a multi-layer TPS 136
Design and testing of a paraffin-based hybrid rocket demonstrator 136
Computational Fluid-Dynamic Simulations of the Internal Ballistics of Hybrid Rocket Burning Paraffin-based Fuel 135
Aerodynamic analysis of a flap-based deployable re-entry system in different flight conditions 134
Preliminary design and study of 5N HTP monopropellant thruster for small satellites 134
CHARACTERIZATION OF CARBON-FIBER REINFORCED ULTRA-HIGH-TEMPERATURE CERAMIC MATRIX COMPOSITES IN ARC-JET ENVIRONMENT 134
Effect of SiC concentration on aero-thermal behavior of ZrB2-based ceramics in hypersonic environment 134
Fast Reconfiguration Maneuvers of a Micro-satellite Constellation Based on a Hybrid Rocket Engine 132
Arc-jet wind tunnel characterization of ultra-high-temperature ceramic matrix composites 132
Propulsion tests on ultra-high-temperature ceramic matrix composites for reusable rocket nozzles 131
MODELLING OF PARAFFIN-BASED FUEL COMBUSTION IN HYBRID ROCKETS 131
Design and Testing of a Paraffin-Based 1000 N HRE Breadboard 130
Experimental investigation of N2O decomposition with pd∕al2 o3 cylindrical pellets catalyst 130
Capillary rising of self-rewetting solutions in laser engraved micro-channels 129
The Small Mars System 126
Self-ReWetting capillary flow under evaporation and condensation processes in parabolic flight conditions 126
Recent advancements in experimental and numerical characterization of paraffin-based fuels for hybrid rocket application 126
The application of computational thermo-fluid-dynamics to the simulation of hybrid rocket internal ballistics with classical or liquefying fuels: A review 126
IRENE - Italian re-entry nacelle for microgravity experiments 125
Upgrading of an Arc-heated Flow Facility for Reentry Simulation 124
Characterization of novel ceramic composites for rocket nozzles in high-temperature harsh environments 124
Regression rate model assessed by ballistic reconstruction technique in hybrid rocket engines burning liquefying fuels 122
CONVENZIONE NATURALE E ALLA MARANGONI IN SISTEMI LIQUIDI PARZIALMENTE MISCIBILI 122
A new firing test campaign on the 1000 N thrust-class Hyprob hybrid rocket engine 121
Aero-Thermo-Dynamic Analysis of a Low Ballistic Coefficient Deployable Capsule in Earth Re-Entry 121
Rarefied aerodynamics of a deployable re-entry capsule 121
Conceptual design of de-orbit and re-entry modules for standard CubeSats 120
Experimental and numerical simulation, by an arc-jet facility, of hypersonic flow in Titan's atmosphere 120
Planetary entry simulation 119
Ultra-High-Temperature Testing of Sintered ZrB2-based Ceramic Composites in Atmospheric Re-entry Environment 119
Compositionally complex catalytic oxide beds free of noble metals for H2O2 fuelled monopropellant thrusters 117
On a more rational specification for the microgravity environment of the International Space Station 117
Self-consistent surface-temperature boundary condition for iquefying-fuel-based hybrid rockets internal-ballistics simulation 117
Hybrid Rocket Engines Design for Materials Characterization 116
Regression Rate and Performance Analysis via Ballistic Reconstruction of a small-scale H2O2-based Hybrid Rocket fuelled by Polyvinyl Chloride 116
Recent development on heat pipes for ground and space applications 116
Adjustable aerobraking heat shield for Satellites deployment and recovery 116
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
Studio aerotermodinamico di sistemi di protezione termica innovativi per velivoli ipersonici 114
Mini-IRENE: The First European Flight Experiment Of A Deployable Heat Shield 114
A study of a high lift wing-body configuration for low earth orbit re-entry. 113
Aerothermodynamic and stability analyses of a deployable re-entry capsule 113
Self rewetting fluids heat transfer experiment selene 113
Aerodynamic study of a 3U CubeSat for drag-based in-plane orbital maneuvers in Very Low Earth Orbit 112
Ground-based activities in preparation of microgravity experiments on heat pipes with self-rewetting fluids 112
An Improvement of the Gas-surface Interaction and Entrainment Models for Paraffin-based Fuels in Hybrid Rocket Engines 112
Fast reconfiguration maneuvers of a micro-satellite constellation based on a hybrid rocket engine 112
Influenza dell'effetto Marangoni sull'efficienza di heat pipes per applicazioni spaziali 111
Self-rewetting heat transfer fluids and nano-brines for space heat pipes 111
ESA Project: Innovative Wickless Heat Pipe Systems for Ground and Space Applications 111
Innovative heat pipes with self-rewetting fluids under normal and reduced gravity conditions 110
Aerothermodynamic and system analysis of a small hypersonic airplane (Hyplane) 110
Effects of solar panels on Aerodynamics of a small satellite with deployable aero-brake 110
Analisi delle prestazioni di ugelli a spina con gas reagenti 109
Precise Re-Entry and Landing of Propellantless Low Earth Orbit Spacecraft 109
Processing and testing of UHTCMCs for aerospace applications 108
Heat pipes with self-rewetting fluids for space applications 108
Heat transfer fluids 108
A simplified computational fluid-dynamic approach to the oxidizer injector design in hybrid rockets 108
Numerical aspects of particle-in-cell simulations for plasma-motion modeling of electric thrusters 108
Heat pipes for space applications 107
Simulation of titan atmosphere by an arc-heated facility 107
The Importance of an accurate knowledge of the Microgravity environment for potential ISS users 106
Heat transfer characteristics of flat plate pulsating heat pipe using self-rewetting fluids 106
Durable oxide catalysts free of noble metals for Hydrogen peroxide thrusters 105
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: Altitude effects on the flowfield structure 105
Totale 14.751
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Categoria #
all - tutte 100.003
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 100.003
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/202146 0 0 0 0 0 0 0 0 0 0 0 46
2021/20221.737 53 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
2025/202613.772 1.425 994 1.245 1.147 2.160 619 1.516 1.136 2.084 889 449 108
Totale 33.485