IRIS
SAVINO, RAFFAELE
 Distribuzione geografica
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Continente #
EU - Europa 9.226
AS - Asia 8.476
NA - Nord America 7.520
SA - Sud America 1.088
AF - Africa 161
OC - Oceania 44
Continente sconosciuto - Info sul continente non disponibili 10
Totale 26.525
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Nazione #
US - Stati Uniti d'America 7.016
SG - Singapore 4.699
IT - Italia 3.082
RU - Federazione Russa 2.931
CN - Cina 1.720
HK - Hong Kong 906
BR - Brasile 868
DE - Germania 680
UA - Ucraina 554
VN - Vietnam 438
CA - Canada 404
GB - Regno Unito 401
FI - Finlandia 354
IE - Irlanda 300
SE - Svezia 239
IN - India 186
NL - Olanda 184
FR - Francia 145
ES - Italia 89
AR - Argentina 88
JP - Giappone 84
KR - Corea 78
MX - Messico 63
AT - Austria 52
TR - Turchia 52
BD - Bangladesh 49
PL - Polonia 48
BE - Belgio 46
EC - Ecuador 38
AU - Australia 35
ID - Indonesia 32
TW - Taiwan 29
CL - Cile 28
ZA - Sudafrica 24
CI - Costa d'Avorio 23
EG - Egitto 23
IQ - Iraq 23
PT - Portogallo 21
PK - Pakistan 20
CO - Colombia 19
PH - Filippine 17
AE - Emirati Arabi Uniti 16
RO - Romania 16
IL - Israele 15
KE - Kenya 15
MA - Marocco 15
UZ - Uzbekistan 14
DZ - Algeria 13
IR - Iran 13
SA - Arabia Saudita 13
PE - Perù 12
BG - Bulgaria 11
CZ - Repubblica Ceca 11
GR - Grecia 11
LT - Lituania 11
VE - Venezuela 11
TH - Thailandia 9
BO - Bolivia 8
PY - Paraguay 8
UY - Uruguay 8
HN - Honduras 7
HU - Ungheria 7
KZ - Kazakistan 7
CH - Svizzera 6
ET - Etiopia 6
EU - Europa 6
GE - Georgia 5
JO - Giordania 5
LB - Libano 5
NZ - Nuova Zelanda 5
QA - Qatar 5
GA - Gabon 4
MY - Malesia 4
NP - Nepal 4
RS - Serbia 4
TJ - Tagikistan 4
TN - Tunisia 4
BS - Bahamas 3
CR - Costa Rica 3
DO - Repubblica Dominicana 3
KG - Kirghizistan 3
KH - Cambogia 3
MG - Madagascar 3
MN - Mongolia 3
NA - Namibia 3
NG - Nigeria 3
NO - Norvegia 3
PA - Panama 3
TT - Trinidad e Tobago 3
A1 - Anonimo 2
AL - Albania 2
AZ - Azerbaigian 2
BB - Barbados 2
BH - Bahrain 2
BN - Brunei Darussalam 2
BW - Botswana 2
BY - Bielorussia 2
BZ - Belize 2
CW - ???statistics.table.value.countryCode.CW??? 2
DK - Danimarca 2
Totale 26.464
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Città #
Singapore 2.096
Chandler 904
Hong Kong 871
Moscow 777
Santa Clara 579
Jacksonville 529
Naples 527
Beijing 375
Napoli 353
Ashburn 321
Millbury 316
Munich 286
Princeton 274
Hefei 258
Montréal 222
Nanjing 208
Los Angeles 186
Boston 176
Ho Chi Minh City 166
Buffalo 154
Rome 151
Mcallen 142
Wilmington 122
Ottawa 117
Woodbridge 106
Amsterdam 104
The Dalles 103
Houston 88
Milan 84
Dallas 82
Des Moines 79
Hanoi 77
Redondo Beach 77
Kronberg 69
Nanchang 69
Ann Arbor 67
São Paulo 67
Centro 59
New York 59
Seattle 59
Hebei 58
Dublin 55
Salerno 52
Cagliari 51
Caserta 51
Boardman 49
Seoul 48
Turin 48
Norwalk 46
Bologna 44
Shenyang 44
Frankfurt am Main 42
Jiaxing 41
Lawrence 38
Helsinki 37
Tianjin 37
Torre Annunziata 37
Changsha 36
Pune 36
Vienna 35
Warsaw 34
Lappeenranta 32
Mexico City 31
Chennai 30
San Francisco 29
Casoria 28
London 28
Rio de Janeiro 28
Taranto 27
Belo Horizonte 26
Falkenstein 26
Madrid 26
Santiago 25
Tokyo 25
Brasília 23
Chicago 23
Haiphong 23
Brooklyn 22
Shanghai 22
Dong Ket 20
Atlanta 19
Kunming 19
Turku 19
Denver 18
Guangzhou 18
Nuremberg 18
Redwood City 18
Da Nang 17
Delft 17
Falls Church 17
Mumbai 17
Stockholm 17
Melbourne 16
Phoenix 16
Roubaix 16
Brussels 15
Sapporo 15
Stuttgart 15
Ankara 14
Buenos Aires 14
Totale 13.107
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Nome #
Aerothermal Analysis of a Sample-Return Reentry Capsule 834
Mini-IRENE: Design Of Deployable Heat Shield Capsule For A Sounding Rocket Flight Experiment 388
FORCE: A FORmation Flying SAR Based on CubEsat Assemblies 251
Two-Hundred-Newton Laboratory-Scale Hybrid Rocket Testing for Paraffin Fuel-Performance Characterization 245
The Small Mars Satellite: a European small-size Mars lander 217
Development and flight test of a suborbital re-entry demonstrator 188
Experimental and numerical assessment of regression rate and propulsive performance of 10N-class hybrid rockets for nanosatellite maneuvering 183
Ultra-High-Temperature Ceramic Matrix Composites for Hybrid Rocket Nozzles 178
Experimental Characterization of an Impulsive Hydrogen Peroxide-based Rocket for Fine Orbit Control 175
Computational Fluid-dynamic Simulations of Hybrid Rocket Internal Flow Including Discharge Nozzle 172
Aerodynamic study of airframe-engine integration of a supersonic business jet 162
Aero-thermo-chemical characterization of ultra-high-temperature ceramics for aerospace applications 160
HYBRID ROCKETS WITH NOZZLE IN ULTRA-HIGH-TEMPERATURE CERAMIC COMPOSITES 160
Design and testing of a monopropellant thruster based on N2O decomposition in Pd/Al2O3 pellets catalytic bed 142
Aerodynamic Control System for a Deployable Re-entry Capsule 139
Hypersonic boost-glide systems: Flight mechanics and plasma parameters evaluation through aero-thermo-chemical computational fluid dynamics 138
Mini Irene Project: Ground Demonstrator Plasma Wind Tunnel Testing 138
Aerodynamic Control System for a Deployable Re-Entry Capsule 137
Experimental characterization of a hydrogen peroxide-based thruster for small satellites 133
Visualization of liquid distribution and dry-out in a single-channel heat pipe with different wettability 131
RODIO Mission Status and Future Developments 129
Aerodynamic Analysis of the Aerospaceplane HYPLANE in Supersonic Rarefied Flow 129
A benchmark study on the thermal conductivity of nanofluids 126
Thermal performance of self-rewetting fluid heat pipe containing dilute solutions of polymer-capped silver nanoparticles synthesized by microwave-polyol process 124
DSMC Aero-Thermo-Dynamic Analysis of a Deployable Capsule for Mars Entry 124
Aerodinamica parte I fondamenti e principi 121
Mixed-Compression Supersonic Intake and Engine–Airframe Integration 120
Assessment of a deployable aerodynamic control system for microsatellites recovery 120
Non-linear aero-elastic response of a multi-layer TPS 115
Design and Testing of a Paraffin-Based 1000 N HRE Breadboard 113
Capillary rising of self-rewetting solutions in laser engraved micro-channels 112
Combined fluid-dynamic modelling of hybrid rocket internal ballistics and nozzle heat transfer 112
Small Mars satellite: A low-cost system for Mars exploration 112
Effect of hypersonic flow chemical composition on the oxidation behavior of a super-strong UHTC 112
Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket 112
Propulsion tests on ultra-high-temperature ceramic matrix composites for reusable rocket nozzles 111
IRENE - Italian re-entry nacelle for microgravity experiments 111
Transient Computational Thermofluid-Dynamic Simulation of Hybrid Rocket Internal Ballistics 111
Aerodynamic analysis of a flap-based deployable re-entry system in different flight conditions 109
Preliminary design and study of 5N HTP monopropellant thruster for small satellites 109
Arc-jet wind tunnel characterization of ultra-high-temperature ceramic matrix composites 109
CONVENZIONE NATURALE E ALLA MARANGONI IN SISTEMI LIQUIDI PARZIALMENTE MISCIBILI 108
The Small Mars System 106
Computational Fluid-Dynamic Simulations of the Internal Ballistics of Hybrid Rocket Burning Paraffin-based Fuel 106
Effect of SiC concentration on aero-thermal behavior of ZrB2-based ceramics in hypersonic environment 106
Recent advancements in experimental and numerical characterization of paraffin-based fuels for hybrid rocket application 104
Upgrading of an Arc-heated Flow Facility for Reentry Simulation 103
Experimental and numerical simulation, by an arc-jet facility, of hypersonic flow in Titan's atmosphere 103
Aero-Thermo-Dynamic Analysis of a Low Ballistic Coefficient Deployable Capsule in Earth Re-Entry 103
Design and testing of a paraffin-based hybrid rocket demonstrator 103
The application of computational thermo-fluid-dynamics to the simulation of hybrid rocket internal ballistics with classical or liquefying fuels: A review 102
MODELLING OF PARAFFIN-BASED FUEL COMBUSTION IN HYBRID ROCKETS 102
Compositionally complex catalytic oxide beds free of noble metals for H2O2 fuelled monopropellant thrusters 101
Conceptual design of de-orbit and re-entry modules for standard CubeSats 101
Aerothermodynamic and system analysis of a small hypersonic airplane (Hyplane) 101
Recent development on heat pipes for ground and space applications 101
CHARACTERIZATION OF CARBON-FIBER REINFORCED ULTRA-HIGH-TEMPERATURE CERAMIC MATRIX COMPOSITES IN ARC-JET ENVIRONMENT 101
Experimental investigation of N2O decomposition with pd∕al2 o3 cylindrical pellets catalyst 101
Influenza dell'effetto Marangoni sull'efficienza di heat pipes per applicazioni spaziali 99
Aerothermodynamic and stability analyses of a deployable re-entry capsule 98
Rarefied aerodynamics of a deployable re-entry capsule 97
Self-consistent surface-temperature boundary condition for iquefying-fuel-based hybrid rockets internal-ballistics simulation 97
A new firing test campaign on the 1000 N thrust-class Hyprob hybrid rocket engine 96
Planetary entry simulation 96
Heat pipes with self-rewetting fluids for space applications 96
Ground-based activities in preparation of microgravity experiments on heat pipes with self-rewetting fluids 96
Self rewetting fluids heat transfer experiment selene 96
Adjustable aerobraking heat shield for Satellites deployment and recovery 96
Ultra-High-Temperature Testing of Sintered ZrB2-based Ceramic Composites in Atmospheric Re-entry Environment 95
Experimental analysis of a Flat Plate Pulsating Heat Pipe with Self-ReWetting Fluids during a parabolic flight campaign 94
Self-ReWetting capillary flow under evaporation and condensation processes in parabolic flight conditions 94
Fast Reconfiguration Maneuvers of a Micro-satellite Constellation Based on a Hybrid Rocket Engine 93
Studio aerotermodinamico di sistemi di protezione termica innovativi per velivoli ipersonici 93
Heat pipes for space applications 93
Characterization of novel ceramic composites for rocket nozzles in high-temperature harsh environments 92
Self-rewetting heat transfer fluids and nano-brines for space heat pipes 91
Spazio: oltre 50 anni di storia in Campania 91
Testing ultra-high -temperature ceramics for thermal protection and rocket applications 91
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: IAD geometrical effects on the flowfield structure 90
Analisi delle prestazioni di ugelli a spina con gas reagenti 90
Mini-IRENE: The First European Flight Experiment Of A Deployable Heat Shield 90
Effects of solar panels on Aerodynamics of a small satellite with deployable aero-brake 90
ESA Project: Innovative Wickless Heat Pipe Systems for Ground and Space Applications 90
Fast reconfiguration maneuvers of a micro-satellite constellation based on a hybrid rocket engine 90
The Fluid-dynamic disturbances induced on the ISS based on the first acceleration measurements on board the Space Station 89
Innovative heat pipes with self-rewetting fluids under normal and reduced gravity conditions 89
Ablation tests on HfC- and TaC-based ceramics for aeropropulsive applications 89
Regression rate model assessed by ballistic reconstruction technique in hybrid rocket engines burning liquefying fuels 88
Preliminary Validation of Fluid-Structure Interaction Modeling for Hypersonic Deployable Re-Entry Systems 88
Heat transfer characteristics of flat plate pulsating heat pipe using self-rewetting fluids 88
An Improvement of the Gas-surface Interaction and Entrainment Models for Paraffin-based Fuels in Hybrid Rocket Engines 88
70 MW plasma wind tunnel up-grades for ESA Aurora TPS testing 87
Experimental set up for characterization of Carbide-based materials in propulsion environment 87
Thermo-chemical surface instabilities of SiC-ZrB 2 ceramics in high enthalpy dissociated supersonic airflows 87
The Importance of an accurate knowledge of the Microgravity environment for potential ISS users 86
Marangoni Heat Pipes: An experiment onboard Italian MIOSAT microsatellite 86
Heat transfer fluids 86
Simulation of titan atmosphere by an arc-heated facility 86
A simplified computational fluid-dynamic approach to the oxidizer injector design in hybrid rockets 86
On a more rational specification for the microgravity environment of the International Space Station 85
Totale 12.293
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Categoria #
all - tutte 84.093
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 84.093
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021879 0 0 0 0 0 193 131 43 222 84 160 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
2025/20267.327 1.425 994 1.245 1.147 2.160 356 0 0 0 0 0 0
Totale 27.040