IRIS
MUNGIGUERRA, STEFANO
 Distribuzione geografica
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Continente #
AS - Asia 3.852
EU - Europa 3.803
NA - Nord America 3.323
SA - Sud America 354
Continente sconosciuto - Info sul continente non disponibili 193
AF - Africa 88
OC - Oceania 21
Totale 11.634
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Nazione #
US - Stati Uniti d'America 3.156
IT - Italia 1.874
SG - Singapore 1.524
RU - Federazione Russa 869
CN - Cina 837
VN - Vietnam 509
HK - Hong Kong 248
DE - Germania 247
BR - Brasile 239
FR - Francia 154
GB - Regno Unito 153
IN - India 139
JP - Giappone 136
BD - Bangladesh 119
CA - Canada 109
NL - Olanda 106
KR - Corea 71
FI - Finlandia 61
UA - Ucraina 56
ES - Italia 53
TW - Taiwan 49
IE - Irlanda 44
AT - Austria 42
AR - Argentina 41
TR - Turchia 34
PH - Filippine 33
PL - Polonia 29
BE - Belgio 25
MX - Messico 24
CL - Cile 21
IQ - Iraq 20
TH - Thailandia 20
CI - Costa d'Avorio 19
AU - Australia 18
ID - Indonesia 18
AE - Emirati Arabi Uniti 14
PT - Portogallo 13
ZA - Sudafrica 13
CO - Colombia 12
EG - Egitto 12
RO - Romania 11
SE - Svezia 11
EC - Ecuador 10
IR - Iran 10
CZ - Repubblica Ceca 9
DZ - Algeria 9
IL - Israele 9
KE - Kenya 9
PE - Perù 9
CH - Svizzera 8
GR - Grecia 8
JM - Giamaica 8
MY - Malesia 8
NP - Nepal 8
VE - Venezuela 8
BO - Bolivia 7
LT - Lituania 7
PK - Pakistan 7
SA - Arabia Saudita 7
CR - Costa Rica 6
KZ - Kazakistan 6
MA - Marocco 6
JO - Giordania 5
HU - Ungheria 4
NI - Nicaragua 4
TN - Tunisia 4
UZ - Uzbekistan 4
EE - Estonia 3
ET - Etiopia 3
HN - Honduras 3
LB - Libano 3
NO - Norvegia 3
NZ - Nuova Zelanda 3
OM - Oman 3
PY - Paraguay 3
SC - Seychelles 3
UY - Uruguay 3
BG - Bulgaria 2
BY - Bielorussia 2
DO - Repubblica Dominicana 2
GP - Guadalupe 2
NA - Namibia 2
SI - Slovenia 2
TZ - Tanzania 2
VC - Saint Vincent e Grenadine 2
AF - Afghanistan, Repubblica islamica di 1
AL - Albania 1
AM - Armenia 1
AO - Angola 1
AZ - Azerbaigian 1
BB - Barbados 1
BH - Bahrain 1
BM - Bermuda 1
BN - Brunei Darussalam 1
BZ - Belize 1
CD - Congo 1
CU - Cuba 1
EU - Europa 1
GT - Guatemala 1
HR - Croazia 1
Totale 11.424
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Città #
Singapore 840
San Jose 543
Naples 437
Ashburn 321
Santa Clara 235
Moscow 225
Hong Kong 218
Hefei 206
Beijing 202
Rome 157
Chandler 155
Ho Chi Minh City 139
Hanoi 109
The Dalles 100
Council Bluffs 97
Munich 93
Milan 89
Los Angeles 87
Tokyo 80
Napoli 70
Lauterbourg 68
New York 52
Turin 50
Mcallen 49
Bologna 48
Salerno 43
Montréal 42
Buffalo 40
Dallas 40
Seoul 36
Phoenix 33
Dublin 32
Lappeenranta 31
Millbury 31
Vienna 31
Boston 30
Des Moines 30
Frankfurt am Main 29
Haiphong 29
Lawrence 29
Amsterdam 24
Centro 24
Seattle 23
São Paulo 21
Nanjing 20
Pune 20
Redondo Beach 20
Madrid 19
Da Nang 18
Wilmington 18
Brooklyn 17
Helsinki 17
Chennai 16
San Francisco 16
Toronto 16
Torre Annunziata 16
Warsaw 16
Changsha 15
Chicago 15
Guangzhou 15
Santiago 15
Caserta 14
Delft 14
Houston 14
Nuremberg 14
Sapporo 14
Shanghai 14
Bangkok 13
Casalnuovo di Napoli 13
Daytona Beach 13
Orem 13
Woodbridge 13
Falkenstein 12
Casoria 11
Hyderabad 11
London 11
Ottawa 11
Bengaluru 10
Cologne 10
Hải Dương 10
Kansas City 10
Kent 10
Orlando 10
Palermo 10
Salò 10
Taipei 10
Torre del Greco 10
Bari 9
Brasília 9
Columbus 9
Fairfield 9
Mexico City 9
Montreal 9
Paris 9
Princeton 9
Villaricca 9
Washington 9
Can Tho 8
Catania 8
City of London 8
Totale 5.976
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Nome #
Mini-IRENE: Design Of Deployable Heat Shield Capsule For A Sounding Rocket Flight Experiment 491
FORCE: A FORmation Flying SAR Based on CubEsat Assemblies 354
RODIO Mission Status and Future Developments 292
Computational Evaluation of Aero-Thermo-Dynamic Loads and Effect of Catalyticity in an Arc-Jet Wind Tunnel 291
Two-Hundred-Newton Laboratory-Scale Hybrid Rocket Testing for Paraffin Fuel-Performance Characterization 290
Development and flight test of a suborbital re-entry demonstrator 266
Experimental and numerical assessment of regression rate and propulsive performance of 10N-class hybrid rockets for nanosatellite maneuvering 261
Fast Reconfiguration Maneuvers of a Micro-satellite Constellation Based on a Hybrid Rocket Engine 239
Experimental Characterization of an Impulsive Hydrogen Peroxide-based Rocket for Fine Orbit Control 228
Computational Fluid-dynamic Simulations of Hybrid Rocket Internal Flow Including Discharge Nozzle 226
Ultra-High-Temperature Ceramic Matrix Composites for Hybrid Rocket Nozzles 219
Aerodynamic study of airframe-engine integration of a supersonic business jet 197
HYBRID ROCKETS WITH NOZZLE IN ULTRA-HIGH-TEMPERATURE CERAMIC COMPOSITES 197
Aero-thermo-chemical characterization of ultra-high-temperature ceramics for aerospace applications 186
Design and testing of a monopropellant thruster based on N2O decomposition in Pd/Al2O3 pellets catalytic bed 171
Experimental characterization of a hydrogen peroxide-based thruster for small satellites 166
Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket 163
Experimental Investigation of Capillary-Driven Two-Phase Flow in Water/Butanol under Reduced Gravity Conditions 161
Assessment of a deployable aerodynamic control system for microsatellites recovery 159
Mini Irene Project: Ground Demonstrator Plasma Wind Tunnel Testing 159
Mixed-Compression Supersonic Intake and Engine–Airframe Integration 156
Effect of SiC concentration on aero-thermal behavior of ZrB2-based ceramics in hypersonic environment 155
Preliminary design and study of 5N HTP monopropellant thruster for small satellites 154
Combined fluid-dynamic modelling of hybrid rocket internal ballistics and nozzle heat transfer 153
Aerodynamic analysis of a flap-based deployable re-entry system in different flight conditions 148
Computational Fluid-Dynamic Simulations of the Internal Ballistics of Hybrid Rocket Burning Paraffin-based Fuel 148
Effect of hypersonic flow chemical composition on the oxidation behavior of a super-strong UHTC 146
Design and testing of a paraffin-based hybrid rocket demonstrator 145
Processing and testing of UHTCMCs for aerospace applications 141
CHARACTERIZATION OF CARBON-FIBER REINFORCED ULTRA-HIGH-TEMPERATURE CERAMIC MATRIX COMPOSITES IN ARC-JET ENVIRONMENT 141
MODELLING OF PARAFFIN-BASED FUEL COMBUSTION IN HYBRID ROCKETS 141
Arc-jet wind tunnel characterization of ultra-high-temperature ceramic matrix composites 140
Self-ReWetting capillary flow under evaporation and condensation processes in parabolic flight conditions 139
Propulsion tests on ultra-high-temperature ceramic matrix composites for reusable rocket nozzles 138
Design and Testing of a Paraffin-Based 1000 N HRE Breadboard 138
The application of computational thermo-fluid-dynamics to the simulation of hybrid rocket internal ballistics with classical or liquefying fuels: A review 135
Aerodynamic study of a 3U CubeSat for drag-based in-plane orbital maneuvers in Very Low Earth Orbit 133
Characterization of novel ceramic composites for rocket nozzles in high-temperature harsh environments 133
Rarefied aerodynamics of a deployable re-entry capsule 130
Recent advancements in experimental and numerical characterization of paraffin-based fuels for hybrid rocket application 130
Ultra-High-Temperature Testing of Sintered ZrB2-based Ceramic Composites in Atmospheric Re-entry Environment 129
Hybrid Rocket Engines Design for Materials Characterization 125
A new firing test campaign on the 1000 N thrust-class Hyprob hybrid rocket engine 124
Regression Rate and Performance Analysis via Ballistic Reconstruction of a small-scale H2O2-based Hybrid Rocket fuelled by Polyvinyl Chloride 123
Compositionally complex catalytic oxide beds free of noble metals for H2O2 fuelled monopropellant thrusters 121
Testing ultra-high -temperature ceramics for thermal protection and rocket applications 120
Fast reconfiguration maneuvers of a micro-satellite constellation based on a hybrid rocket engine 119
An Improvement of the Gas-surface Interaction and Entrainment Models for Paraffin-based Fuels in Hybrid Rocket Engines 118
Fuel Ignition in HTP Hybrid Rockets at Very Low Mass Fluxes: Challenges and Pulsed Preheating Techniques Using Palladium-Coated Catalysts 117
Effects of solar panels on Aerodynamics of a small satellite with deployable aero-brake 117
Performance analysis of different air intakes for ABEP in VLEO and evaluation of scale effects 116
Testing and Characterization of Near-Zero-Ablation Fibre-reinforced Ultra High Temperature Ceramics for Aerospace 112
Effect of grain length on GOx-paraffin hybrid rocket engines performance and regression rate 111
Tests and simulations on 200N paraffin-oxygen hybrid rocket engines with different fuel grain lengths 109
Fuel Characterization, Performance Assessment and Thermal Analysis of a Hydrogen Peroxide-based Hybrid Thruster for CubeSats 109
Durable oxide catalysts free of noble metals for Hydrogen peroxide thrusters 107
Study on Aerodynamic Stability of a Deployable Aerobraking Re-entry Capsule 107
Testing 1kN Paraffin-Based Hybrid Rocket Engine 105
Aero-thermo-dynamic Characterization of Large-scale Near-zero Ablation Thermal Protection Systems in Ultra-High-Temperature Ceramic Matrix Composites 104
New Entrainment Model for Modelling the Regression Rate in Hybrid Rocket Engines 99
Ultra-High-Temperature Ceramic Matrix Composites in Hybrid Rocket Propulsion Environment 97
Improved aero-thermal resistance capabilities of ZrB2-based ceramics in hypersonic environment for increasing SiC content 97
Quasi-Optimal Guidance and Control in Very Low Earth Orbit via Deep Learning for Drag-Based Collision Avoidance 96
Firing Tests and Simulations of a CubeSat-Scale H2O2-Based Hybrid Rocket 87
Effect of PAN-based and pitch-based carbon fibres on microstructure and properties of continuous Cf/ZrB2-SiC UHTCMCs 85
null 82
Test and simulation in high-enthalpy atmospheric re-entry conditions of Multi-Phase Ultra-High-Temperature Ceramics 81
Qualification and reusability of long and short fibre-reinforced ultra-refractory composites for aerospace thermal protection systems 77
Aerodynamics and flight mechanics activities for a suborbital flight test of a deployable heat shield capsule 75
Experimental Firing Test Campaign and Nozzle Heat Transfer Reconstruction in a 200 N Hybrid Rocket Engine with Different Paraffin-Based Fuel Grain Lengths 73
Properties and Behavior of 3D-Printed ABS Fuel in a 10 N Hybrid Rocket: Experimental and Numerical Insights 69
Novel Insights on Fluid Dynamics and Performance of 10N-class HTP-based Hybrid Thrusters 66
Failure tolerant functionally graded fiber-reinforced UHTCs exposed to hypersonic flows 66
Elevated temperature performance: Arc-Jet testing of carbon fiber reinforced ZrB₂ bars up to 2200 °C for strength retention assessment 63
Experimental activities on the paraffin-based fuel MTM in the framework of the PHAEDRA project 63
Heat Transfer analysis of Ultra High Temperature Ceramic in High Enthalpy Supersonic Flows 57
Design and Testing of a Hybrid Rocket for Small Spacecraft 44
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 40
Advancements in ultra-high temperature ceramic matrix composites for extreme environments 40
Numerical and experimental analysis of a 200 N class GOX-ABS hybrid rocket engine 40
Pitch stability considerations of 3 U cubesats for differential drag exploitation in VLEO 39
Numerical investigation of critical aspects for the intake of atmosphere-breathing electric propulsions for VLEO applications 37
Ultra-High Temperature Ceramic Matrix Composites: Their Performance in Relevant Environments 36
Relevant Fluid Dynamics Aspects of the Internal Ballistics in a Small-Scale Hybrid Thruster 35
Hypersonic Entry Flow Simulation for Mars Exploration 34
A Novel Versatile Test Bench for Liquid Bipropellant Rocket Testing and Numerical Combustion Simulations 34
Aerodynamic Performance of Flap-Based Deployable Heat Shield for Satellite Reentry and Recovery 30
Digital light processing (DLP) 3D-printed Pd/Al₂O₃ catalysts for H₂O₂ decomposition: towards efficient green thrusters 29
Mini-IRENE, a Successful Re-entry Flight of a Deployable Heatshield Capsule 25
Searching the limits of compositionally complex AlB2-type diboride solid solutions for hypersonic applications 24
Re-Entry Comparison of a Spacecraft in Low Earth Orbit: Propulsion-Assisted vs. Non-Propulsive Configurations 21
Aerothermodynamic response of ZrB2-based compositionally complex ultra-high-temperature ceramics in hypersonic and supersonic flow conditions 18
Performance Degradation and Regeneration of Palladium Catalysts for Hybrid Rockets 15
Mini-IRENE, a successful re-entry flight of a deployable heatshield capsule 7
Totale 11.634
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Categoria #
all - tutte 33.576
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 33.576
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022309 0 0 0 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
2025/20265.209 441 383 436 448 714 169 603 397 715 334 251 318
2026/2027982 198 290 345 149 0 0 0 0 0 0 0 0
Totale 11.634