IRIS
SAVINO, RAFFAELE
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
EU - Europa 9.264
AS - Asia 8.767
NA - Nord America 7.636
SA - Sud America 1.092
AF - Africa 164
OC - Oceania 45
Continente sconosciuto - Info sul continente non disponibili 10
Totale 26.978
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 7.130
SG - Singapore 4.943
IT - Italia 3.094
RU - Federazione Russa 2.933
CN - Cina 1.750
HK - Hong Kong 910
BR - Brasile 872
DE - Germania 684
UA - Ucraina 556
VN - Vietnam 438
CA - Canada 404
GB - Regno Unito 404
FI - Finlandia 354
IE - Irlanda 300
SE - Svezia 239
IN - India 189
NL - Olanda 186
FR - Francia 148
ES - Italia 98
AR - Argentina 88
JP - Giappone 87
KR - Corea 78
MX - Messico 65
AT - Austria 53
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
IQ - Iraq 24
ZA - Sudafrica 24
CI - Costa d'Avorio 23
EG - Egitto 23
PT - Portogallo 21
PK - Pakistan 20
CO - Colombia 19
PH - Filippine 18
IL - Israele 17
AE - Emirati Arabi Uniti 16
KE - Kenya 16
RO - Romania 16
DZ - Algeria 15
MA - Marocco 15
IR - Iran 14
UZ - Uzbekistan 14
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
NZ - Nuova Zelanda 6
GE - Georgia 5
JO - Giordania 5
LB - Libano 5
MY - Malesia 5
NP - Nepal 5
QA - Qatar 5
GA - Gabon 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 26.917
Salva come PNG Salva come JPEG
Città #
Singapore 2.217
Chandler 904
Hong Kong 875
Moscow 777
Santa Clara 580
Naples 532
Jacksonville 529
Beijing 379
Napoli 353
Ashburn 337
Millbury 316
Munich 286
Princeton 274
Hefei 258
Montréal 222
Nanjing 208
Los Angeles 188
Boston 176
Ho Chi Minh City 166
Buffalo 154
Rome 151
Mcallen 142
Wilmington 122
Ottawa 117
The Dalles 115
Woodbridge 106
Amsterdam 104
Houston 88
Milan 84
Dallas 82
Des Moines 79
Hanoi 77
Redondo Beach 77
San Jose 77
Kronberg 69
Nanchang 69
São Paulo 68
Ann Arbor 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
Frankfurt am Main 45
Bologna 44
Shenyang 44
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
Tokyo 26
Santiago 25
Chicago 24
Brasília 23
Haiphong 23
Brooklyn 22
Shanghai 22
Dong Ket 20
Atlanta 19
Kunming 19
Nuremberg 19
Turku 19
Denver 18
Guangzhou 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
Totale 13.342
Salva come PNG Salva come JPEG
Nome #
Aerothermal Analysis of a Sample-Return Reentry Capsule 834
Mini-IRENE: Design Of Deployable Heat Shield Capsule For A Sounding Rocket Flight Experiment 393
FORCE: A FORmation Flying SAR Based on CubEsat Assemblies 255
Two-Hundred-Newton Laboratory-Scale Hybrid Rocket Testing for Paraffin Fuel-Performance Characterization 247
The Small Mars Satellite: a European small-size Mars lander 218
Development and flight test of a suborbital re-entry demonstrator 195
Experimental and numerical assessment of regression rate and propulsive performance of 10N-class hybrid rockets for nanosatellite maneuvering 188
Ultra-High-Temperature Ceramic Matrix Composites for Hybrid Rocket Nozzles 180
Experimental Characterization of an Impulsive Hydrogen Peroxide-based Rocket for Fine Orbit Control 178
Computational Fluid-dynamic Simulations of Hybrid Rocket Internal Flow Including Discharge Nozzle 174
Aerodynamic study of airframe-engine integration of a supersonic business jet 164
HYBRID ROCKETS WITH NOZZLE IN ULTRA-HIGH-TEMPERATURE CERAMIC COMPOSITES 163
Aero-thermo-chemical characterization of ultra-high-temperature ceramics for aerospace applications 160
Design and testing of a monopropellant thruster based on N2O decomposition in Pd/Al2O3 pellets catalytic bed 144
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 138
Experimental characterization of a hydrogen peroxide-based thruster for small satellites 135
Visualization of liquid distribution and dry-out in a single-channel heat pipe with different wettability 131
Aerodynamic Analysis of the Aerospaceplane HYPLANE in Supersonic Rarefied Flow 130
RODIO Mission Status and Future Developments 129
A benchmark study on the thermal conductivity of nanofluids 128
Aerodinamica parte I fondamenti e principi 125
DSMC Aero-Thermo-Dynamic Analysis of a Deployable Capsule for Mars Entry 125
Thermal performance of self-rewetting fluid heat pipe containing dilute solutions of polymer-capped silver nanoparticles synthesized by microwave-polyol process 124
Assessment of a deployable aerodynamic control system for microsatellites recovery 123
Mixed-Compression Supersonic Intake and Engine–Airframe Integration 122
Non-linear aero-elastic response of a multi-layer TPS 115
Combined fluid-dynamic modelling of hybrid rocket internal ballistics and nozzle heat transfer 115
Effect of hypersonic flow chemical composition on the oxidation behavior of a super-strong UHTC 115
IRENE - Italian re-entry nacelle for microgravity experiments 114
Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket 114
Capillary rising of self-rewetting solutions in laser engraved micro-channels 113
Transient Computational Thermofluid-Dynamic Simulation of Hybrid Rocket Internal Ballistics 113
Small Mars satellite: A low-cost system for Mars exploration 113
Design and Testing of a Paraffin-Based 1000 N HRE Breadboard 113
Aerodynamic analysis of a flap-based deployable re-entry system in different flight conditions 112
Effect of SiC concentration on aero-thermal behavior of ZrB2-based ceramics in hypersonic environment 112
Propulsion tests on ultra-high-temperature ceramic matrix composites for reusable rocket nozzles 111
Preliminary design and study of 5N HTP monopropellant thruster for small satellites 111
Arc-jet wind tunnel characterization of ultra-high-temperature ceramic matrix composites 110
CONVENZIONE NATURALE E ALLA MARANGONI IN SISTEMI LIQUIDI PARZIALMENTE MISCIBILI 109
The Small Mars System 108
Computational Fluid-Dynamic Simulations of the Internal Ballistics of Hybrid Rocket Burning Paraffin-based Fuel 107
Upgrading of an Arc-heated Flow Facility for Reentry Simulation 105
Design and testing of a paraffin-based hybrid rocket demonstrator 105
Recent advancements in experimental and numerical characterization of paraffin-based fuels for hybrid rocket application 105
The application of computational thermo-fluid-dynamics to the simulation of hybrid rocket internal ballistics with classical or liquefying fuels: A review 105
MODELLING OF PARAFFIN-BASED FUEL COMBUSTION IN HYBRID ROCKETS 105
Aero-Thermo-Dynamic Analysis of a Low Ballistic Coefficient Deployable Capsule in Earth Re-Entry 104
Compositionally complex catalytic oxide beds free of noble metals for H2O2 fuelled monopropellant thrusters 103
Experimental and numerical simulation, by an arc-jet facility, of hypersonic flow in Titan's atmosphere 103
Experimental investigation of N2O decomposition with pd∕al2 o3 cylindrical pellets catalyst 102
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
Influenza dell'effetto Marangoni sull'efficienza di heat pipes per applicazioni spaziali 100
Rarefied aerodynamics of a deployable re-entry capsule 99
Self-consistent surface-temperature boundary condition for iquefying-fuel-based hybrid rockets internal-ballistics simulation 99
Planetary entry simulation 98
Aerothermodynamic and stability analyses of a deployable re-entry capsule 98
Regression rate model assessed by ballistic reconstruction technique in hybrid rocket engines burning liquefying fuels 97
A new firing test campaign on the 1000 N thrust-class Hyprob hybrid rocket engine 97
Heat pipes with self-rewetting fluids for space applications 97
Ground-based activities in preparation of microgravity experiments on heat pipes with self-rewetting fluids 97
Self rewetting fluids heat transfer experiment selene 97
Adjustable aerobraking heat shield for Satellites deployment and recovery 97
Self-ReWetting capillary flow under evaporation and condensation processes in parabolic flight conditions 97
Studio aerotermodinamico di sistemi di protezione termica innovativi per velivoli ipersonici 96
Ultra-High-Temperature Testing of Sintered ZrB2-based Ceramic Composites in Atmospheric Re-entry Environment 96
Fast Reconfiguration Maneuvers of a Micro-satellite Constellation Based on a Hybrid Rocket Engine 95
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: IAD geometrical effects on the flowfield structure 95
Heat pipes for space applications 95
Experimental analysis of a Flat Plate Pulsating Heat Pipe with Self-ReWetting Fluids during a parabolic flight campaign 94
Mini-IRENE: The First European Flight Experiment Of A Deployable Heat Shield 93
Effects of solar panels on Aerodynamics of a small satellite with deployable aero-brake 93
Testing ultra-high -temperature ceramics for thermal protection and rocket applications 93
Characterization of novel ceramic composites for rocket nozzles in high-temperature harsh environments 93
Self-rewetting heat transfer fluids and nano-brines for space heat pipes 92
Spazio: oltre 50 anni di storia in Campania 92
Analisi delle prestazioni di ugelli a spina con gas reagenti 91
ESA Project: Innovative Wickless Heat Pipe Systems for Ground and Space Applications 91
Fast reconfiguration maneuvers of a micro-satellite constellation based on a hybrid rocket engine 91
Innovative heat pipes with self-rewetting fluids under normal and reduced gravity conditions 90
Heat transfer fluids 90
An Improvement of the Gas-surface Interaction and Entrainment Models for Paraffin-based Fuels in Hybrid Rocket Engines 90
The Fluid-dynamic disturbances induced on the ISS based on the first acceleration measurements on board the Space Station 89
On a more rational specification for the microgravity environment of the International Space Station 89
Ablation tests on HfC- and TaC-based ceramics for aeropropulsive applications 89
The Importance of an accurate knowledge of the Microgravity environment for potential ISS users 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
A simplified computational fluid-dynamic approach to the oxidizer injector design in hybrid rockets 88
Regression Rate and Performance Analysis via Ballistic Reconstruction of a small-scale H2O2-based Hybrid Rocket fuelled by Polyvinyl Chloride 87
70 MW plasma wind tunnel up-grades for ESA Aurora TPS testing 87
A study of a high lift wing-body configuration for low earth orbit re-entry. 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
Totale 12.461
Salva come PNG Salva come JPEG
Categoria #
all - tutte 86.102
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 86.102
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021686 0 0 0 0 0 0 131 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
2025/20267.797 1.425 994 1.245 1.147 2.160 619 207 0 0 0 0 0
Totale 27.510