IRIS
MUNGIGUERRA, STEFANO
 Distribuzione geografica
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Continente #
EU - Europa 1.920
NA - Nord America 1.221
AS - Asia 752
SA - Sud America 41
AF - Africa 26
OC - Oceania 12
Continente sconosciuto - Info sul continente non disponibili 1
Totale 3.973
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Nazione #
IT - Italia 1.265
US - Stati Uniti d'America 1.155
SG - Singapore 294
CN - Cina 150
HK - Hong Kong 138
DE - Germania 134
GB - Regno Unito 95
RU - Federazione Russa 71
CA - Canada 64
IN - India 60
NL - Olanda 51
FI - Finlandia 50
UA - Ucraina 50
IE - Irlanda 43
AT - Austria 32
JP - Giappone 28
FR - Francia 25
ES - Italia 23
BR - Brasile 22
BE - Belgio 20
CI - Costa d'Avorio 17
TR - Turchia 16
CL - Cile 14
TW - Taiwan 13
PT - Portogallo 12
AU - Australia 11
RO - Romania 10
CZ - Repubblica Ceca 9
ID - Indonesia 9
PH - Filippine 9
PL - Polonia 8
GR - Grecia 7
KR - Corea 7
SE - Svezia 7
EG - Egitto 6
IR - Iran 5
TH - Thailandia 5
AE - Emirati Arabi Uniti 4
BO - Bolivia 4
IL - Israele 4
LT - Lituania 3
JO - Giordania 2
NO - Norvegia 2
SA - Arabia Saudita 2
TZ - Tanzania 2
BG - Bulgaria 1
CO - Colombia 1
DO - Repubblica Dominicana 1
EU - Europa 1
IQ - Iraq 1
KZ - Kazakistan 1
LB - Libano 1
MA - Marocco 1
MC - Monaco 1
MX - Messico 1
NP - Nepal 1
NZ - Nuova Zelanda 1
PK - Pakistan 1
SI - Slovenia 1
UZ - Uzbekistan 1
Totale 3.973
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Città #
Naples 295
Santa Clara 204
Singapore 168
Chandler 155
Hong Kong 122
Ashburn 89
Rome 77
Napoli 70
Munich 61
Milan 55
Mcallen 49
Montréal 42
Beijing 39
Salerno 39
Bologna 35
Turin 33
Dublin 31
Lappeenranta 31
Millbury 31
Des Moines 28
Lawrence 28
Vienna 28
Boston 24
Centro 24
Seattle 22
Nanjing 18
Pune 18
Torre Annunziata 16
Amsterdam 15
Wilmington 15
Caserta 14
Helsinki 14
Casalnuovo di Napoli 13
Santiago 13
Woodbridge 13
Casoria 11
Cologne 10
Ottawa 10
Salò 10
Torre del Greco 10
Dallas 9
Daytona Beach 9
Fairfield 9
Falkenstein 9
Princeton 9
The Dalles 9
Villaricca 9
Qualiano 8
Redwood City 8
Casalecchio di Reno 7
Changsha 7
Giugliano in Campania 7
Hyderabad 7
London 7
Moscow 7
Orlando 7
Sant Joan Despí 7
Shanghai 7
Tokyo 7
Al Qāhirah al Jadīdah 6
Arzano 6
Aversa 6
Braunschweig 6
Brussels 6
Carinola 6
Chennai 6
Guangzhou 6
Leicester 6
Leuven 6
Melito di Napoli 6
Norwalk 6
Portici 6
Potenza 6
Avellino 5
Bangkok 5
Cagliari 5
Catania 5
Frattamaggiore 5
Hebei 5
Houston 5
Hsinchu County 5
Huntsville 5
Izmir 5
Katsushika 5
Lecce 5
Leverano 5
Limatola 5
Montecorvino Rovella 5
Mumbai 5
Padova 5
Paris 5
Pompei 5
Sapporo 5
Stuttgart 5
Sydney 5
Taipei 5
Toulouse 5
Bari 4
Boardman 4
Bucharest 4
Totale 2.345
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Nome #
Mini-IRENE: Design Of Deployable Heat Shield Capsule For A Sounding Rocket Flight Experiment 275
Computational Evaluation of Aero-Thermo-Dynamic Loads and Effect of Catalyticity in an Arc-Jet Wind Tunnel 238
Two-Hundred-Newton Laboratory-Scale Hybrid Rocket Testing for Paraffin Fuel-Performance Characterization 184
FORCE: A FORmation Flying SAR Based on CubEsat Assemblies 168
Aero-thermo-chemical characterization of ultra-high-temperature ceramics for aerospace applications 128
Ultra-High-Temperature Ceramic Matrix Composites for Hybrid Rocket Nozzles 125
Experimental and numerical assessment of regression rate and propulsive performance of 10N-class hybrid rockets for nanosatellite maneuvering 103
Computational Fluid-dynamic Simulations of Hybrid Rocket Internal Flow Including Discharge Nozzle 100
Development and flight test of a suborbital re-entry demonstrator 95
Experimental Characterization of an Impulsive Hydrogen Peroxide-based Rocket for Fine Orbit Control 91
Mini Irene Project: Ground Demonstrator Plasma Wind Tunnel Testing 91
HYBRID ROCKETS WITH NOZZLE IN ULTRA-HIGH-TEMPERATURE CERAMIC COMPOSITES 90
Aerodynamic study of airframe-engine integration of a supersonic business jet 88
Arc-jet wind tunnel characterization of ultra-high-temperature ceramic matrix composites 68
CHARACTERIZATION OF CARBON-FIBER REINFORCED ULTRA-HIGH-TEMPERATURE CERAMIC MATRIX COMPOSITES IN ARC-JET ENVIRONMENT 68
Design and testing of a monopropellant thruster based on N2O decomposition in Pd/Al2O3 pellets catalytic bed 66
Design and Testing of a Paraffin-Based 1000 N HRE Breadboard 65
Experimental characterization of a hydrogen peroxide-based thruster for small satellites 64
Aero-thermo-dynamic Characterization of Large-scale Near-zero Ablation Thermal Protection Systems in Ultra-High-Temperature Ceramic Matrix Composites 62
Mixed-Compression Supersonic Intake and Engine–Airframe Integration 60
Assessment of a deployable aerodynamic control system for microsatellites recovery 60
Experimental Investigation of Capillary-Driven Two-Phase Flow in Water/Butanol under Reduced Gravity Conditions 59
Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket 57
Combined fluid-dynamic modelling of hybrid rocket internal ballistics and nozzle heat transfer 56
Preliminary design and study of 5N HTP monopropellant thruster for small satellites 55
Effect of hypersonic flow chemical composition on the oxidation behavior of a super-strong UHTC 55
Rarefied aerodynamics of a deployable re-entry capsule 54
Design and testing of a paraffin-based hybrid rocket demonstrator 54
Ultra-High-Temperature Ceramic Matrix Composites in Hybrid Rocket Propulsion Environment 53
MODELLING OF PARAFFIN-BASED FUEL COMBUSTION IN HYBRID ROCKETS 53
Computational Fluid-Dynamic Simulations of the Internal Ballistics of Hybrid Rocket Burning Paraffin-based Fuel 52
Effect of SiC concentration on aero-thermal behavior of ZrB2-based ceramics in hypersonic environment 51
Recent advancements in experimental and numerical characterization of paraffin-based fuels for hybrid rocket application 50
Improved aero-thermal resistance capabilities of ZrB2-based ceramics in hypersonic environment for increasing SiC content 50
Propulsion tests on ultra-high-temperature ceramic matrix composites for reusable rocket nozzles 49
Testing ultra-high -temperature ceramics for thermal protection and rocket applications 49
Ultra-High-Temperature Testing of Sintered ZrB2-based Ceramic Composites in Atmospheric Re-entry Environment 48
Effects of solar panels on Aerodynamics of a small satellite with deployable aero-brake 46
Characterization of novel ceramic composites for rocket nozzles in high-temperature harsh environments 46
Aerodynamic analysis of a flap-based deployable re-entry system in different flight conditions 45
Self-ReWetting capillary flow under evaporation and condensation processes in parabolic flight conditions 44
Testing and Characterization of Near-Zero-Ablation Fibre-reinforced Ultra High Temperature Ceramics for Aerospace 43
The application of computational thermo-fluid-dynamics to the simulation of hybrid rocket internal ballistics with classical or liquefying fuels: A review 43
A new firing test campaign on the 1000 N thrust-class Hyprob hybrid rocket engine 42
Study on Aerodynamic Stability of a Deployable Aerobraking Re-entry Capsule 42
Fast reconfiguration maneuvers of a micro-satellite constellation based on a hybrid rocket engine 42
Compositionally complex catalytic oxide beds free of noble metals for H2O2 fuelled monopropellant thrusters 41
Effect of grain length on GOx-paraffin hybrid rocket engines performance and regression rate 39
An Improvement of the Gas-surface Interaction and Entrainment Models for Paraffin-based Fuels in Hybrid Rocket Engines 38
Effect of PAN-based and pitch-based carbon fibres on microstructure and properties of continuous Cf/ZrB2-SiC UHTCMCs 38
Mini-IRENE, a successful re-entry flight of a deployable heatshield capsule 37
Testing 1kN Paraffin-Based Hybrid Rocket Engine 36
Tests and simulations on 200N paraffin-oxygen hybrid rocket engines with different fuel grain lengths 30
New Entrainment Model for Modelling the Regression Rate in Hybrid Rocket Engines 29
Fuel Characterization, Performance Assessment and Thermal Analysis of a Hydrogen Peroxide-based Hybrid Thruster for CubeSats 29
Qualification and reusability of long and short fibre-reinforced ultra-refractory composites for aerospace thermal protection systems 27
Regression Rate and Performance Analysis via Ballistic Reconstruction of a small-scale H2O2-based Hybrid Rocket fuelled by Polyvinyl Chloride 25
Hybrid Rocket Engines Design for Materials Characterization 24
Aerodynamics and flight mechanics activities for a suborbital flight test of a deployable heat shield capsule 23
Performance analysis of different air intakes for ABEP in VLEO and evaluation of scale effects 22
Experimental Firing Test Campaign and Nozzle Heat Transfer Reconstruction in a 200 N Hybrid Rocket Engine with Different Paraffin-Based Fuel Grain Lengths 21
Failure tolerant functionally graded fiber-reinforced UHTCs exposed to hypersonic flows 21
Fast Reconfiguration Maneuvers of a Micro-satellite Constellation Based on a Hybrid Rocket Engine 20
Durable oxide catalysts free of noble metals for Hydrogen peroxide thrusters 19
Test and simulation in high-enthalpy atmospheric re-entry conditions of Multi-Phase Ultra-High-Temperature Ceramics 19
Fuel Ignition in HTP Hybrid Rockets at Very Low Mass Fluxes: Challenges and Pulsed Preheating Techniques Using Palladium-Coated Catalysts 18
Processing and testing of UHTCMCs for aerospace applications 18
Experimental activities on the paraffin-based fuel MTM in the framework of the PHAEDRA project 14
Elevated temperature performance: Arc-Jet testing of carbon fiber reinforced ZrB₂ bars up to 2200 °C for strength retention assessment 13
Totale 4.128
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Categoria #
all - tutte 13.743
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 13.743
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020174 0 0 0 0 0 0 0 0 34 64 58 18
2020/2021275 17 9 32 27 11 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
2024/20251.367 120 156 74 82 162 218 275 239 41 0 0 0
Totale 4.128