IRIS
MUNGIGUERRA, STEFANO
 Distribuzione geografica
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Continente #
EU - Europa 3.223
AS - Asia 2.714
NA - Nord America 1.766
SA - Sud America 285
AF - Africa 62
OC - Oceania 19
Continente sconosciuto - Info sul continente non disponibili 1
Totale 8.070
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Nazione #
US - Stati Uniti d'America 1.662
IT - Italia 1.497
SG - Singapore 1.336
RU - Federazione Russa 866
CN - Cina 715
DE - Germania 217
HK - Hong Kong 200
BR - Brasile 199
GB - Regno Unito 128
VN - Vietnam 109
NL - Olanda 94
IN - India 90
CA - Canada 77
FR - Francia 67
FI - Finlandia 60
KR - Corea 57
UA - Ucraina 54
ES - Italia 47
JP - Giappone 45
IE - Irlanda 44
AT - Austria 41
AR - Argentina 34
TR - Turchia 28
PL - Polonia 21
TW - Taiwan 21
BE - Belgio 20
CI - Costa d'Avorio 18
MX - Messico 18
AU - Australia 16
CL - Cile 16
PH - Filippine 14
AE - Emirati Arabi Uniti 13
ID - Indonesia 13
BD - Bangladesh 12
PT - Portogallo 12
RO - Romania 10
CZ - Repubblica Ceca 9
EG - Egitto 9
SE - Svezia 9
EC - Ecuador 8
IL - Israele 8
IR - Iran 8
KE - Kenya 8
ZA - Sudafrica 8
CO - Colombia 7
GR - Grecia 7
IQ - Iraq 7
PE - Perù 7
BO - Bolivia 6
DZ - Algeria 6
LT - Lituania 6
TH - Thailandia 6
VE - Venezuela 5
HU - Ungheria 4
MA - Marocco 4
MY - Malesia 4
PK - Pakistan 4
SA - Arabia Saudita 4
HN - Honduras 3
NP - Nepal 3
NZ - Nuova Zelanda 3
UZ - Uzbekistan 3
CH - Svizzera 2
JO - Giordania 2
KZ - Kazakistan 2
NA - Namibia 2
NO - Norvegia 2
PY - Paraguay 2
TZ - Tanzania 2
AF - Afghanistan, Repubblica islamica di 1
AL - Albania 1
AZ - Azerbaigian 1
BG - Bulgaria 1
BH - Bahrain 1
BN - Brunei Darussalam 1
BZ - Belize 1
CD - Congo 1
CR - Costa Rica 1
CU - Cuba 1
DO - Repubblica Dominicana 1
ET - Etiopia 1
EU - Europa 1
GP - Guadalupe 1
HR - Croazia 1
KG - Kirghizistan 1
KH - Cambogia 1
LB - Libano 1
LY - Libia 1
MC - Monaco 1
MK - Macedonia 1
NE - Niger 1
OM - Oman 1
SI - Slovenia 1
SN - Senegal 1
TJ - Tagikistan 1
TL - Timor Orientale 1
UY - Uruguay 1
VC - Saint Vincent e Grenadine 1
Totale 8.070
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Città #
Singapore 689
Naples 358
Moscow 224
Santa Clara 212
Hefei 206
Hong Kong 183
Beijing 178
Chandler 155
Ashburn 154
Rome 100
Munich 93
San Jose 71
Napoli 70
Milan 67
The Dalles 56
Los Angeles 54
Mcallen 49
Bologna 42
Ho Chi Minh City 42
Montréal 42
Salerno 42
Turin 36
Seoul 35
Dublin 32
Lappeenranta 31
Millbury 31
Vienna 31
Des Moines 29
Boston 28
Lawrence 28
Dallas 26
Buffalo 24
Centro 24
Frankfurt am Main 23
Seattle 23
Amsterdam 20
Nanjing 20
New York 20
Redondo Beach 20
Pune 18
Helsinki 16
Torre Annunziata 16
Wilmington 16
Warsaw 15
Caserta 14
Changsha 14
Delft 14
Guangzhou 14
Hanoi 14
Madrid 14
Santiago 14
Casalnuovo di Napoli 13
São Paulo 13
Woodbridge 13
Daytona Beach 12
Falkenstein 12
Shanghai 12
Casoria 11
Chennai 11
Chicago 11
Nuremberg 11
San Francisco 11
Tokyo 11
Cologne 10
Haiphong 10
London 10
Ottawa 10
Salò 10
Torre del Greco 10
Bari 9
Fairfield 9
Princeton 9
Sapporo 9
Villaricca 9
Brasília 8
Houston 8
Leeuwarden 8
Qualiano 8
Redwood City 8
Turku 8
Brooklyn 7
Casalecchio di Reno 7
Giugliano in Campania 7
Hyderabad 7
Jakarta 7
Kobe 7
Montreal 7
Mumbai 7
Orlando 7
Paris 7
Sant Joan Despí 7
Tianjin 7
Abu Dhabi 6
Al Qāhirah al Jadīdah 6
Ankara 6
Arzano 6
Aversa 6
Bangkok 6
Belo Horizonte 6
Braunschweig 6
Totale 4.173
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Nome #
Mini-IRENE: Design Of Deployable Heat Shield Capsule For A Sounding Rocket Flight Experiment 394
Computational Evaluation of Aero-Thermo-Dynamic Loads and Effect of Catalyticity in an Arc-Jet Wind Tunnel 263
FORCE: A FORmation Flying SAR Based on CubEsat Assemblies 255
Two-Hundred-Newton Laboratory-Scale Hybrid Rocket Testing for Paraffin Fuel-Performance Characterization 248
Development and flight test of a suborbital re-entry demonstrator 196
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 181
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 175
Aerodynamic study of airframe-engine integration of a supersonic business jet 164
HYBRID ROCKETS WITH NOZZLE IN ULTRA-HIGH-TEMPERATURE CERAMIC COMPOSITES 164
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 145
Experimental characterization of a hydrogen peroxide-based thruster for small satellites 140
Mini Irene Project: Ground Demonstrator Plasma Wind Tunnel Testing 138
RODIO Mission Status and Future Developments 129
Experimental Investigation of Capillary-Driven Two-Phase Flow in Water/Butanol under Reduced Gravity Conditions 125
Assessment of a deployable aerodynamic control system for microsatellites recovery 123
Mixed-Compression Supersonic Intake and Engine–Airframe Integration 122
Effect of hypersonic flow chemical composition on the oxidation behavior of a super-strong UHTC 117
Combined fluid-dynamic modelling of hybrid rocket internal ballistics and nozzle heat transfer 116
Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket 116
Arc-jet wind tunnel characterization of ultra-high-temperature ceramic matrix composites 114
Design and Testing of a Paraffin-Based 1000 N HRE Breadboard 114
Aerodynamic analysis of a flap-based deployable re-entry system in different flight conditions 113
Effect of SiC concentration on aero-thermal behavior of ZrB2-based ceramics in hypersonic environment 113
Preliminary design and study of 5N HTP monopropellant thruster for small satellites 112
Propulsion tests on ultra-high-temperature ceramic matrix composites for reusable rocket nozzles 111
The application of computational thermo-fluid-dynamics to the simulation of hybrid rocket internal ballistics with classical or liquefying fuels: A review 109
Computational Fluid-Dynamic Simulations of the Internal Ballistics of Hybrid Rocket Burning Paraffin-based Fuel 108
MODELLING OF PARAFFIN-BASED FUEL COMBUSTION IN HYBRID ROCKETS 108
Design and testing of a paraffin-based hybrid rocket demonstrator 106
Recent advancements in experimental and numerical characterization of paraffin-based fuels for hybrid rocket application 105
Compositionally complex catalytic oxide beds free of noble metals for H2O2 fuelled monopropellant thrusters 103
Fast Reconfiguration Maneuvers of a Micro-satellite Constellation Based on a Hybrid Rocket Engine 102
CHARACTERIZATION OF CARBON-FIBER REINFORCED ULTRA-HIGH-TEMPERATURE CERAMIC MATRIX COMPOSITES IN ARC-JET ENVIRONMENT 102
Rarefied aerodynamics of a deployable re-entry capsule 100
Self-ReWetting capillary flow under evaporation and condensation processes in parabolic flight conditions 98
A new firing test campaign on the 1000 N thrust-class Hyprob hybrid rocket engine 97
Characterization of novel ceramic composites for rocket nozzles in high-temperature harsh environments 97
Ultra-High-Temperature Testing of Sintered ZrB2-based Ceramic Composites in Atmospheric Re-entry Environment 96
Effects of solar panels on Aerodynamics of a small satellite with deployable aero-brake 94
Testing ultra-high -temperature ceramics for thermal protection and rocket applications 94
Performance analysis of different air intakes for ABEP in VLEO and evaluation of scale effects 92
Fast reconfiguration maneuvers of a micro-satellite constellation based on a hybrid rocket engine 91
An Improvement of the Gas-surface Interaction and Entrainment Models for Paraffin-based Fuels in Hybrid Rocket Engines 90
Hybrid Rocket Engines Design for Materials Characterization 88
Durable oxide catalysts free of noble metals for Hydrogen peroxide thrusters 87
Regression Rate and Performance Analysis via Ballistic Reconstruction of a small-scale H2O2-based Hybrid Rocket fuelled by Polyvinyl Chloride 87
Study on Aerodynamic Stability of a Deployable Aerobraking Re-entry Capsule 86
Aero-thermo-dynamic Characterization of Large-scale Near-zero Ablation Thermal Protection Systems in Ultra-High-Temperature Ceramic Matrix Composites 86
Tests and simulations on 200N paraffin-oxygen hybrid rocket engines with different fuel grain lengths 85
Testing 1kN Paraffin-Based Hybrid Rocket Engine 85
Testing and Characterization of Near-Zero-Ablation Fibre-reinforced Ultra High Temperature Ceramics for Aerospace 83
Effect of grain length on GOx-paraffin hybrid rocket engines performance and regression rate 83
Fuel Ignition in HTP Hybrid Rockets at Very Low Mass Fluxes: Challenges and Pulsed Preheating Techniques Using Palladium-Coated Catalysts 79
Ultra-High-Temperature Ceramic Matrix Composites in Hybrid Rocket Propulsion Environment 78
Improved aero-thermal resistance capabilities of ZrB2-based ceramics in hypersonic environment for increasing SiC content 77
Mini-IRENE, a successful re-entry flight of a deployable heatshield capsule 75
New Entrainment Model for Modelling the Regression Rate in Hybrid Rocket Engines 75
Fuel Characterization, Performance Assessment and Thermal Analysis of a Hydrogen Peroxide-based Hybrid Thruster for CubeSats 75
Effect of PAN-based and pitch-based carbon fibres on microstructure and properties of continuous Cf/ZrB2-SiC UHTCMCs 66
Processing and testing of UHTCMCs for aerospace applications 64
Test and simulation in high-enthalpy atmospheric re-entry conditions of Multi-Phase Ultra-High-Temperature Ceramics 64
Aerodynamic study of a 3U CubeSat for drag-based in-plane orbital maneuvers in Very Low Earth Orbit 60
Aerodynamics and flight mechanics activities for a suborbital flight test of a deployable heat shield capsule 60
Experimental Firing Test Campaign and Nozzle Heat Transfer Reconstruction in a 200 N Hybrid Rocket Engine with Different Paraffin-Based Fuel Grain Lengths 53
Elevated temperature performance: Arc-Jet testing of carbon fiber reinforced ZrB₂ bars up to 2200 °C for strength retention assessment 50
Qualification and reusability of long and short fibre-reinforced ultra-refractory composites for aerospace thermal protection systems 49
Failure tolerant functionally graded fiber-reinforced UHTCs exposed to hypersonic flows 47
Experimental activities on the paraffin-based fuel MTM in the framework of the PHAEDRA project 43
Quasi-Optimal Guidance and Control in Very Low Earth Orbit via Deep Learning for Drag-Based Collision Avoidance 38
Properties and Behavior of 3D-Printed ABS Fuel in a 10 N Hybrid Rocket: Experimental and Numerical Insights 36
Novel Insights on Fluid Dynamics and Performance of 10N-class HTP-based Hybrid Thrusters 22
Hypersonic Entry Flow Simulation for Mars Exploration 10
Firing Tests and Simulations of a CubeSat-Scale H2O2-Based Hybrid Rocket 7
Advancements in ultra-high temperature ceramic matrix composites for extreme environments 7
Heat Transfer analysis of Ultra High Temperature Ceramic in High Enthalpy Supersonic Flows 7
Numerical and experimental analysis of a 200 N class GOX-ABS hybrid rocket engine 6
A Novel Versatile Test Bench for Liquid Bipropellant Rocket Testing and Numerical Combustion Simulations 4
Design and Testing of a Hybrid Rocket for Small Spacecraft 4
Numerical investigation of critical aspects for the intake of atmosphere-breathing electric propulsions for VLEO applications 3
Mini-IRENE, a Successful Re-entry Flight of a Deployable Heatshield Capsule 3
Relevant Fluid Dynamics Aspects of the Internal Ballistics in a Small-Scale Hybrid Thruster 3
Digital light processing (DLP) 3D-printed Pd/Al₂O₃ catalysts for H₂O₂ decomposition: towards efficient green thrusters 3
Ageing and Space Qualification of Ultra-High Temperature Ceramic Matrix Composites for Next-Generation Thermal Protection Systems: From Ground Testing to Low Earth Orbit Environment 2
Ultra-High Temperature Ceramic Matrix Composites: Their Performance in Relevant Environments 2
Totale 8.248
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Categoria #
all - tutte 23.111
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 23.111
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021150 0 0 0 0 0 0 12 15 50 47 20 6
2021/2022343 16 6 12 20 2 24 9 22 39 22 76 95
2022/2023578 39 45 22 26 69 72 26 68 74 19 86 32
2023/2024964 42 68 48 71 84 118 83 100 44 94 132 80
2024/20252.682 120 156 74 82 162 218 275 239 186 184 768 218
2025/20262.805 441 383 436 448 714 169 214 0 0 0 0 0
Totale 8.248