IRIS
MUNGIGUERRA, STEFANO
 Distribuzione geografica
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Continente #
EU - Europa 3.184
AS - Asia 2.599
NA - Nord America 1.648
SA - Sud America 283
AF - Africa 60
OC - Oceania 18
Continente sconosciuto - Info sul continente non disponibili 1
Totale 7.793
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Nazione #
US - Stati Uniti d'America 1.546
IT - Italia 1.479
SG - Singapore 1.249
RU - Federazione Russa 864
CN - Cina 697
DE - Germania 214
HK - Hong Kong 200
BR - Brasile 197
GB - Regno Unito 124
VN - Vietnam 109
NL - Olanda 92
IN - India 89
CA - Canada 77
FR - Francia 64
FI - Finlandia 60
KR - Corea 57
UA - Ucraina 52
IE - Irlanda 44
ES - Italia 42
JP - Giappone 42
AT - Austria 41
AR - Argentina 34
TR - Turchia 28
PL - Polonia 21
TW - Taiwan 21
BE - Belgio 20
CI - Costa d'Avorio 18
AU - Australia 16
CL - Cile 16
MX - Messico 16
AE - Emirati Arabi Uniti 13
ID - Indonesia 13
PH - Filippine 13
BD - Bangladesh 12
PT - Portogallo 12
RO - Romania 10
CZ - Repubblica Ceca 9
EG - Egitto 9
SE - Svezia 9
EC - Ecuador 8
ZA - Sudafrica 8
CO - Colombia 7
GR - Grecia 7
IQ - Iraq 7
IR - Iran 7
KE - Kenya 7
PE - Perù 7
BO - Bolivia 6
IL - Israele 6
LT - Lituania 6
TH - Thailandia 6
DZ - Algeria 5
VE - Venezuela 5
HU - Ungheria 4
MA - Marocco 4
PK - Pakistan 4
SA - Arabia Saudita 4
HN - Honduras 3
MY - Malesia 3
UZ - Uzbekistan 3
CH - Svizzera 2
JO - Giordania 2
KZ - Kazakistan 2
NA - Namibia 2
NO - Norvegia 2
NP - Nepal 2
NZ - Nuova Zelanda 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 7.793
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Città #
Singapore 611
Naples 354
Moscow 224
Santa Clara 212
Hefei 206
Hong Kong 183
Beijing 176
Chandler 155
Ashburn 141
Rome 95
Munich 93
Napoli 70
Milan 67
Los Angeles 54
Mcallen 49
Bologna 42
Ho Chi Minh City 42
Montréal 42
Salerno 42
Turin 36
Seoul 35
The Dalles 33
Dublin 32
Lappeenranta 31
Millbury 31
Vienna 31
Des Moines 29
Boston 28
Lawrence 28
Dallas 26
Buffalo 24
Centro 24
Seattle 23
Amsterdam 20
Frankfurt am Main 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
Woodbridge 13
Daytona Beach 12
Falkenstein 12
Shanghai 12
São Paulo 12
Casoria 11
Chennai 11
Chicago 11
Nuremberg 11
San Francisco 11
Cologne 10
Haiphong 10
London 10
Ottawa 10
Salò 10
Tokyo 10
Torre del Greco 10
Fairfield 9
Princeton 9
Sapporo 9
Villaricca 9
Brasília 8
Houston 8
Leeuwarden 8
Qualiano 8
Redwood City 8
Turku 8
Bari 7
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
Abu Dhabi 6
Al Qāhirah al Jadīdah 6
Ankara 6
Arzano 6
Aversa 6
Bangkok 6
Belo Horizonte 6
Braunschweig 6
Brussels 6
Buenos Aires 6
Totale 3.975
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Nome #
Mini-IRENE: Design Of Deployable Heat Shield Capsule For A Sounding Rocket Flight Experiment 388
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 251
Two-Hundred-Newton Laboratory-Scale Hybrid Rocket Testing for Paraffin Fuel-Performance Characterization 245
Development and flight test of a suborbital re-entry demonstrator 186
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 161
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
Mini Irene Project: Ground Demonstrator Plasma Wind Tunnel Testing 138
Experimental characterization of a hydrogen peroxide-based thruster for small satellites 133
RODIO Mission Status and Future Developments 129
Mixed-Compression Supersonic Intake and Engine–Airframe Integration 120
Assessment of a deployable aerodynamic control system for microsatellites recovery 120
Experimental Investigation of Capillary-Driven Two-Phase Flow in Water/Butanol under Reduced Gravity Conditions 120
Design and Testing of a Paraffin-Based 1000 N HRE Breadboard 113
Combined fluid-dynamic modelling of hybrid rocket internal ballistics and nozzle heat transfer 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
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
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
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
CHARACTERIZATION OF CARBON-FIBER REINFORCED ULTRA-HIGH-TEMPERATURE CERAMIC MATRIX COMPOSITES IN ARC-JET ENVIRONMENT 101
Rarefied aerodynamics of a deployable re-entry capsule 97
A new firing test campaign on the 1000 N thrust-class Hyprob hybrid rocket engine 96
Ultra-High-Temperature Testing of Sintered ZrB2-based Ceramic Composites in Atmospheric Re-entry Environment 95
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
Characterization of novel ceramic composites for rocket nozzles in high-temperature harsh environments 92
Performance analysis of different air intakes for ABEP in VLEO and evaluation of scale effects 91
Testing ultra-high -temperature ceramics for thermal protection and rocket applications 91
Effects of solar panels on Aerodynamics of a small satellite with deployable aero-brake 90
Fast reconfiguration maneuvers of a micro-satellite constellation based on a hybrid rocket engine 90
An Improvement of the Gas-surface Interaction and Entrainment Models for Paraffin-based Fuels in Hybrid Rocket Engines 88
Aero-thermo-dynamic Characterization of Large-scale Near-zero Ablation Thermal Protection Systems in Ultra-High-Temperature Ceramic Matrix Composites 85
Study on Aerodynamic Stability of a Deployable Aerobraking Re-entry Capsule 84
Hybrid Rocket Engines Design for Materials Characterization 83
Regression Rate and Performance Analysis via Ballistic Reconstruction of a small-scale H2O2-based Hybrid Rocket fuelled by Polyvinyl Chloride 83
Testing and Characterization of Near-Zero-Ablation Fibre-reinforced Ultra High Temperature Ceramics for Aerospace 83
Testing 1kN Paraffin-Based Hybrid Rocket Engine 82
Effect of grain length on GOx-paraffin hybrid rocket engines performance and regression rate 81
Durable oxide catalysts free of noble metals for Hydrogen peroxide thrusters 80
Tests and simulations on 200N paraffin-oxygen hybrid rocket engines with different fuel grain lengths 79
Improved aero-thermal resistance capabilities of ZrB2-based ceramics in hypersonic environment for increasing SiC content 76
Fuel Ignition in HTP Hybrid Rockets at Very Low Mass Fluxes: Challenges and Pulsed Preheating Techniques Using Palladium-Coated Catalysts 75
Ultra-High-Temperature Ceramic Matrix Composites in Hybrid Rocket Propulsion Environment 75
Mini-IRENE, a successful re-entry flight of a deployable heatshield capsule 74
Fuel Characterization, Performance Assessment and Thermal Analysis of a Hydrogen Peroxide-based Hybrid Thruster for CubeSats 71
New Entrainment Model for Modelling the Regression Rate in Hybrid Rocket Engines 69
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 59
Aerodynamics and flight mechanics activities for a suborbital flight test of a deployable heat shield capsule 59
Experimental Firing Test Campaign and Nozzle Heat Transfer Reconstruction in a 200 N Hybrid Rocket Engine with Different Paraffin-Based Fuel Grain Lengths 51
Elevated temperature performance: Arc-Jet testing of carbon fiber reinforced ZrB₂ bars up to 2200 °C for strength retention assessment 49
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 34
Properties and Behavior of 3D-Printed ABS Fuel in a 10 N Hybrid Rocket: Experimental and Numerical Insights 34
Totale 7.952
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Categoria #
all - tutte 22.102
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 22.102
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021179 0 0 0 0 0 29 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
2025/20262.509 441 383 436 448 714 87 0 0 0 0 0 0
Totale 7.952