IRIS
MUNGIGUERRA, STEFANO
 Distribuzione geografica
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Continente #
AS - Asia 3.687
EU - Europa 3.563
NA - Nord America 2.492
SA - Sud America 339
AF - Africa 85
OC - Oceania 19
Continente sconosciuto - Info sul continente non disponibili 1
Totale 10.186
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Nazione #
US - Stati Uniti d'America 2.359
IT - Italia 1.676
SG - Singapore 1.519
RU - Federazione Russa 869
CN - Cina 816
VN - Vietnam 504
HK - Hong Kong 245
DE - Germania 242
BR - Brasile 228
FR - Francia 150
GB - Regno Unito 144
JP - Giappone 127
IN - India 119
NL - Olanda 100
CA - Canada 93
KR - Corea 70
FI - Finlandia 61
UA - Ucraina 55
ES - Italia 52
IE - Irlanda 44
TW - Taiwan 42
AT - Austria 41
AR - Argentina 40
BD - Bangladesh 39
TR - Turchia 34
PH - Filippine 30
BE - Belgio 24
MX - Messico 24
PL - Polonia 22
CL - Cile 21
IQ - Iraq 20
TH - Thailandia 20
CI - Costa d'Avorio 19
ID - Indonesia 17
AU - Australia 16
AE - Emirati Arabi Uniti 14
PT - Portogallo 13
ZA - Sudafrica 13
EG - Egitto 12
SE - Svezia 11
CO - Colombia 10
EC - Ecuador 10
RO - Romania 10
CZ - Repubblica Ceca 9
DZ - Algeria 9
IL - Israele 9
IR - Iran 9
KE - Kenya 9
CH - Svizzera 8
MY - Malesia 8
PE - Perù 8
VE - Venezuela 8
BO - Bolivia 7
GR - Grecia 7
LT - Lituania 7
PK - Pakistan 7
MA - Marocco 6
SA - Arabia Saudita 6
JO - Giordania 5
NP - Nepal 5
HU - Ungheria 4
TN - Tunisia 4
UZ - Uzbekistan 4
ET - Etiopia 3
HN - Honduras 3
JM - Giamaica 3
LB - Libano 3
NO - Norvegia 3
NZ - Nuova Zelanda 3
OM - Oman 3
PY - Paraguay 3
UY - Uruguay 3
BG - Bulgaria 2
CR - Costa Rica 2
DO - Repubblica Dominicana 2
KZ - Kazakistan 2
NA - Namibia 2
SI - Slovenia 2
TZ - Tanzania 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
BN - Brunei Darussalam 1
BY - Bielorussia 1
BZ - Belize 1
CD - Congo 1
CU - Cuba 1
EE - Estonia 1
EU - Europa 1
GP - Guadalupe 1
HR - Croazia 1
KG - Kirghizistan 1
KH - Cambogia 1
LV - Lettonia 1
LY - Libia 1
MC - Monaco 1
Totale 10.176
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Città #
Singapore 836
Naples 399
San Jose 385
Moscow 225
Ashburn 221
Santa Clara 220
Hong Kong 216
Hefei 206
Beijing 202
Chandler 155
Ho Chi Minh City 138
Rome 125
Hanoi 106
The Dalles 100
Munich 93
Milan 77
Tokyo 76
Napoli 70
Lauterbourg 68
Los Angeles 67
Mcallen 49
New York 46
Turin 46
Bologna 44
Salerno 43
Montréal 42
Seoul 36
Dallas 33
Dublin 32
Buffalo 31
Lappeenranta 31
Millbury 31
Vienna 31
Boston 29
Des Moines 29
Frankfurt am Main 29
Haiphong 29
Lawrence 29
Council Bluffs 26
Amsterdam 24
Centro 24
Seattle 23
Nanjing 20
Pune 20
Redondo Beach 20
Da Nang 18
Madrid 18
Helsinki 17
Torre Annunziata 16
Warsaw 16
Wilmington 16
Changsha 15
Chennai 15
Guangzhou 15
Santiago 15
São Paulo 15
Caserta 14
Delft 14
Shanghai 14
Bangkok 13
Casalnuovo di Napoli 13
Nuremberg 13
San Francisco 13
Woodbridge 13
Daytona Beach 12
Falkenstein 12
Houston 12
Toronto 12
Brooklyn 11
Casoria 11
Chicago 11
London 11
Cologne 10
Hyderabad 10
Hải Dương 10
Orem 10
Ottawa 10
Palermo 10
Phoenix 10
Salò 10
Sapporo 10
Torre del Greco 10
Bari 9
Fairfield 9
Kansas City 9
Mexico City 9
Orlando 9
Paris 9
Princeton 9
Villaricca 9
Brasília 8
Can Tho 8
City of London 8
Leeuwarden 8
Montreal 8
Neubiberg 8
Qualiano 8
Redwood City 8
Turku 8
Baghdad 7
Totale 5.408
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Nome #
Mini-IRENE: Design Of Deployable Heat Shield Capsule For A Sounding Rocket Flight Experiment 463
FORCE: A FORmation Flying SAR Based on CubEsat Assemblies 295
Two-Hundred-Newton Laboratory-Scale Hybrid Rocket Testing for Paraffin Fuel-Performance Characterization 281
Computational Evaluation of Aero-Thermo-Dynamic Loads and Effect of Catalyticity in an Arc-Jet Wind Tunnel 281
Development and flight test of a suborbital re-entry demonstrator 238
Experimental and numerical assessment of regression rate and propulsive performance of 10N-class hybrid rockets for nanosatellite maneuvering 231
Ultra-High-Temperature Ceramic Matrix Composites for Hybrid Rocket Nozzles 211
Experimental Characterization of an Impulsive Hydrogen Peroxide-based Rocket for Fine Orbit Control 208
Computational Fluid-dynamic Simulations of Hybrid Rocket Internal Flow Including Discharge Nozzle 205
Aerodynamic study of airframe-engine integration of a supersonic business jet 192
RODIO Mission Status and Future Developments 191
HYBRID ROCKETS WITH NOZZLE IN ULTRA-HIGH-TEMPERATURE CERAMIC COMPOSITES 186
Aero-thermo-chemical characterization of ultra-high-temperature ceramics for aerospace applications 179
Design and testing of a monopropellant thruster based on N2O decomposition in Pd/Al2O3 pellets catalytic bed 162
Experimental characterization of a hydrogen peroxide-based thruster for small satellites 157
Mini Irene Project: Ground Demonstrator Plasma Wind Tunnel Testing 154
Experimental Investigation of Capillary-Driven Two-Phase Flow in Water/Butanol under Reduced Gravity Conditions 149
Assessment of a deployable aerodynamic control system for microsatellites recovery 147
Combined fluid-dynamic modelling of hybrid rocket internal ballistics and nozzle heat transfer 146
Mixed-Compression Supersonic Intake and Engine–Airframe Integration 143
Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket 143
Effect of hypersonic flow chemical composition on the oxidation behavior of a super-strong UHTC 138
Design and testing of a paraffin-based hybrid rocket demonstrator 136
Computational Fluid-Dynamic Simulations of the Internal Ballistics of Hybrid Rocket Burning Paraffin-based Fuel 135
Aerodynamic analysis of a flap-based deployable re-entry system in different flight conditions 134
Preliminary design and study of 5N HTP monopropellant thruster for small satellites 134
CHARACTERIZATION OF CARBON-FIBER REINFORCED ULTRA-HIGH-TEMPERATURE CERAMIC MATRIX COMPOSITES IN ARC-JET ENVIRONMENT 134
Effect of SiC concentration on aero-thermal behavior of ZrB2-based ceramics in hypersonic environment 134
Fast Reconfiguration Maneuvers of a Micro-satellite Constellation Based on a Hybrid Rocket Engine 132
Arc-jet wind tunnel characterization of ultra-high-temperature ceramic matrix composites 132
Propulsion tests on ultra-high-temperature ceramic matrix composites for reusable rocket nozzles 131
MODELLING OF PARAFFIN-BASED FUEL COMBUSTION IN HYBRID ROCKETS 131
Design and Testing of a Paraffin-Based 1000 N HRE Breadboard 130
Self-ReWetting capillary flow under evaporation and condensation processes in parabolic flight conditions 126
Recent advancements in experimental and numerical characterization of paraffin-based fuels for hybrid rocket application 126
The application of computational thermo-fluid-dynamics to the simulation of hybrid rocket internal ballistics with classical or liquefying fuels: A review 126
Characterization of novel ceramic composites for rocket nozzles in high-temperature harsh environments 124
A new firing test campaign on the 1000 N thrust-class Hyprob hybrid rocket engine 121
Rarefied aerodynamics of a deployable re-entry capsule 121
Ultra-High-Temperature Testing of Sintered ZrB2-based Ceramic Composites in Atmospheric Re-entry Environment 119
Compositionally complex catalytic oxide beds free of noble metals for H2O2 fuelled monopropellant thrusters 117
Hybrid Rocket Engines Design for Materials Characterization 116
Regression Rate and Performance Analysis via Ballistic Reconstruction of a small-scale H2O2-based Hybrid Rocket fuelled by Polyvinyl Chloride 116
Testing ultra-high -temperature ceramics for thermal protection and rocket applications 115
Aerodynamic study of a 3U CubeSat for drag-based in-plane orbital maneuvers in Very Low Earth Orbit 112
An Improvement of the Gas-surface Interaction and Entrainment Models for Paraffin-based Fuels in Hybrid Rocket Engines 112
Fast reconfiguration maneuvers of a micro-satellite constellation based on a hybrid rocket engine 112
Performance analysis of different air intakes for ABEP in VLEO and evaluation of scale effects 110
Effects of solar panels on Aerodynamics of a small satellite with deployable aero-brake 110
Processing and testing of UHTCMCs for aerospace applications 108
Durable oxide catalysts free of noble metals for Hydrogen peroxide thrusters 105
Fuel Ignition in HTP Hybrid Rockets at Very Low Mass Fluxes: Challenges and Pulsed Preheating Techniques Using Palladium-Coated Catalysts 104
Tests and simulations on 200N paraffin-oxygen hybrid rocket engines with different fuel grain lengths 103
Fuel Characterization, Performance Assessment and Thermal Analysis of a Hydrogen Peroxide-based Hybrid Thruster for CubeSats 103
Study on Aerodynamic Stability of a Deployable Aerobraking Re-entry Capsule 101
Testing 1kN Paraffin-Based Hybrid Rocket Engine 101
Aero-thermo-dynamic Characterization of Large-scale Near-zero Ablation Thermal Protection Systems in Ultra-High-Temperature Ceramic Matrix Composites 100
Testing and Characterization of Near-Zero-Ablation Fibre-reinforced Ultra High Temperature Ceramics for Aerospace 98
Effect of grain length on GOx-paraffin hybrid rocket engines performance and regression rate 98
Ultra-High-Temperature Ceramic Matrix Composites in Hybrid Rocket Propulsion Environment 91
New Entrainment Model for Modelling the Regression Rate in Hybrid Rocket Engines 90
Improved aero-thermal resistance capabilities of ZrB2-based ceramics in hypersonic environment for increasing SiC content 89
null 82
Effect of PAN-based and pitch-based carbon fibres on microstructure and properties of continuous Cf/ZrB2-SiC UHTCMCs 80
Test and simulation in high-enthalpy atmospheric re-entry conditions of Multi-Phase Ultra-High-Temperature Ceramics 74
Aerodynamics and flight mechanics activities for a suborbital flight test of a deployable heat shield capsule 70
Qualification and reusability of long and short fibre-reinforced ultra-refractory composites for aerospace thermal protection systems 65
Experimental Firing Test Campaign and Nozzle Heat Transfer Reconstruction in a 200 N Hybrid Rocket Engine with Different Paraffin-Based Fuel Grain Lengths 64
Failure tolerant functionally graded fiber-reinforced UHTCs exposed to hypersonic flows 62
Quasi-Optimal Guidance and Control in Very Low Earth Orbit via Deep Learning for Drag-Based Collision Avoidance 61
Properties and Behavior of 3D-Printed ABS Fuel in a 10 N Hybrid Rocket: Experimental and Numerical Insights 61
Elevated temperature performance: Arc-Jet testing of carbon fiber reinforced ZrB₂ bars up to 2200 °C for strength retention assessment 58
Novel Insights on Fluid Dynamics and Performance of 10N-class HTP-based Hybrid Thrusters 57
Firing Tests and Simulations of a CubeSat-Scale H2O2-Based Hybrid Rocket 55
Experimental activities on the paraffin-based fuel MTM in the framework of the PHAEDRA project 49
Heat Transfer analysis of Ultra High Temperature Ceramic in High Enthalpy Supersonic Flows 41
Advancements in ultra-high temperature ceramic matrix composites for extreme environments 31
Numerical and experimental analysis of a 200 N class GOX-ABS hybrid rocket engine 31
Hypersonic Entry Flow Simulation for Mars Exploration 30
A Novel Versatile Test Bench for Liquid Bipropellant Rocket Testing and Numerical Combustion Simulations 29
Design and Testing of a Hybrid Rocket for Small Spacecraft 27
Relevant Fluid Dynamics Aspects of the Internal Ballistics in a Small-Scale Hybrid Thruster 26
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 25
Ultra-High Temperature Ceramic Matrix Composites: Their Performance in Relevant Environments 23
Digital light processing (DLP) 3D-printed Pd/Al₂O₃ catalysts for H₂O₂ decomposition: towards efficient green thrusters 23
Pitch stability considerations of 3 U cubesats for differential drag exploitation in VLEO 22
Numerical investigation of critical aspects for the intake of atmosphere-breathing electric propulsions for VLEO applications 21
Mini-IRENE, a Successful Re-entry Flight of a Deployable Heatshield Capsule 20
Re-Entry Comparison of a Spacecraft in Low Earth Orbit: Propulsion-Assisted vs. Non-Propulsive Configurations 14
Searching the limits of compositionally complex AlB2-type diboride solid solutions for hypersonic applications 13
Aerodynamic Performance of Flap-Based Deployable Heat Shield for Satellite Reentry and Recovery 13
Aerothermodynamic response of ZrB2-based compositionally complex ultra-high-temperature ceramics in hypersonic and supersonic flow conditions 10
Performance Degradation and Regeneration of Palladium Catalysts for Hybrid Rockets 3
Totale 10.377
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Categoria #
all - tutte 27.872
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 27.872
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20216 0 0 0 0 0 0 0 0 0 0 0 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
2025/20264.934 441 383 436 448 714 169 603 397 715 334 251 43
Totale 10.377