RE.PUBLIC@POLIMI pubblicazioni di ricerca del Politecnico di Milano

MAGGI, FILIPPO
 Distribuzione geografica
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Continente #
EU - Europa 14.261
NA - Nord America 14.182
AS - Asia 7.294
SA - Sud America 1.317
AF - Africa 334
OC - Oceania 50
Continente sconosciuto - Info sul continente non disponibili 6
Totale 37.444
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Nazione #
US - Stati Uniti d'America 13.797
RU - Federazione Russa 5.327
IT - Italia 4.772
SG - Singapore 2.199
CN - Cina 2.142
BR - Brasile 1.114
VN - Vietnam 940
FR - Francia 659
DE - Germania 638
KR - Corea 490
GB - Regno Unito 431
UA - Ucraina 391
SE - Svezia 352
JP - Giappone 347
FI - Finlandia 336
NL - Olanda 313
CA - Canada 283
IE - Irlanda 280
ES - Italia 232
AT - Austria 226
IN - India 224
HK - Hong Kong 122
MA - Marocco 101
PH - Filippine 94
JO - Giordania 91
CI - Costa d'Avorio 84
TR - Turchia 83
BD - Bangladesh 81
ID - Indonesia 80
PL - Polonia 72
AR - Argentina 68
CH - Svizzera 62
MX - Messico 59
TW - Taiwan 57
ZA - Sudafrica 55
IQ - Iraq 52
BE - Belgio 47
IR - Iran 38
PK - Pakistan 37
EC - Ecuador 33
SA - Arabia Saudita 33
IL - Israele 28
NZ - Nuova Zelanda 27
VE - Venezuela 24
AU - Australia 23
KZ - Kazakistan 23
PT - Portogallo 23
GR - Grecia 21
CO - Colombia 20
EG - Egitto 20
UZ - Uzbekistan 19
CL - Cile 18
AZ - Azerbaigian 17
KE - Kenya 17
DZ - Algeria 15
NP - Nepal 14
PY - Paraguay 14
AE - Emirati Arabi Uniti 13
BG - Bulgaria 12
MY - Malesia 12
TH - Thailandia 12
BO - Bolivia 11
LT - Lituania 11
DO - Repubblica Dominicana 9
CZ - Repubblica Ceca 8
PE - Perù 8
RO - Romania 8
MU - Mauritius 7
TN - Tunisia 7
ET - Etiopia 6
AL - Albania 5
BJ - Benin 5
CR - Costa Rica 5
DK - Danimarca 5
KG - Kirghizistan 5
OM - Oman 5
PA - Panama 5
QA - Qatar 5
TT - Trinidad e Tobago 5
UY - Uruguay 5
AM - Armenia 4
LB - Libano 4
LV - Lettonia 4
SN - Senegal 4
XK - ???statistics.table.value.countryCode.XK??? 4
AO - Angola 3
BA - Bosnia-Erzegovina 3
BB - Barbados 3
BH - Bahrain 3
HU - Ungheria 3
LK - Sri Lanka 3
LU - Lussemburgo 3
NG - Nigeria 3
PS - Palestinian Territory 3
BN - Brunei Darussalam 2
BY - Bielorussia 2
BZ - Belize 2
EU - Europa 2
GD - Grenada 2
HN - Honduras 2
Totale 37.398
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Città #
Milan 1.906
Ashburn 1.846
San Jose 1.328
Singapore 1.232
Fairfield 968
Woodbridge 823
Chandler 796
Moscow 681
Santa Clara 605
Wilmington 499
Hefei 487
Houston 475
Ann Arbor 474
Seoul 432
Seattle 385
The Dalles 368
Cambridge 348
Council Bluffs 339
Beijing 331
Tokyo 293
Dallas 292
Dublin 269
Boardman 234
Jacksonville 224
Lauterbourg 204
Dong Ket 197
Dearborn 195
Vienna 195
Ho Chi Minh City 188
Los Angeles 185
Lawrence 184
Medford 180
Málaga 180
Ottawa 180
Helsinki 158
Rome 147
New York 137
Hanoi 135
Amsterdam 134
North Charleston 131
Buffalo 123
Hong Kong 93
Amman 90
Redwood City 87
Frankfurt am Main 85
Abidjan 82
São Paulo 81
Des Moines 79
Davao City 69
Orem 68
Jakarta 61
Ciampino 57
Giussano 57
Chennai 54
Rho 53
Las Vegas 52
Changsha 51
Warsaw 51
London 49
Turin 48
Falkenstein 47
San Diego 47
Kent 45
Monza 45
Shanghai 45
Chicago 44
Casablanca 43
Pedrengo 43
Bern 42
Kenitra 42
Gavirate 41
Boltiere 40
Marnate 39
Taipei 39
Bovisio Masciago 38
Brussels 37
Montreal 35
Parma 35
Redmond 35
Mumbai 34
Phoenix 34
Rio de Janeiro 34
Stuttgart 34
Istanbul 33
Denver 32
Guangzhou 32
Nanjing 31
Washington 31
Stockholm 30
Zibido San Giacomo 30
Bresso 29
Norwalk 29
Lappeenranta 28
Basingstoke 26
Brooklyn 25
Da Nang 25
Haiphong 25
Hangzhou 25
Johannesburg 25
Belo Horizonte 24
Totale 21.153
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Nome #
Evaluating New Liquid Storable Bipropellants: Safety and Performance Assessments 356
Accelerated ageing of micron- and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity 333
Effect of amide-based compounds on the combustion characteristics of composite solid rocket propellants 309
Aluminum powders: aging effects on metal content and thermogravimetry reactivity 296
A Critical Analysis of Paraffin-based Fuel Formulations for Hybrid Rocket Propulsion 295
Activated Aluminum Powders for Space Propulsion 293
Experimental investigation of paraffin-based fuels for hybrid rocket propulsion 292
A method for mechanical activation of powders by means of balls 286
Iron oxide as solid propellant catalyst: A detailed characterization 282
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 281
Aerospace Propulsion Research Activities at SPlab. Overview and Results 280
Paraffin-Based Fuels and Energetic Additives for Hybrid Rocket Propulsion 267
A parametric study of electrodes geometries for atmospheric electrohydrodynamic propulsion 260
Characterization of SRM plumes with alumina particulate in subscale testing 258
Experimental data from ramjet/scramjet combustion and numerical validation perspectives 257
Development of an intrusive technique for particles collection in rockets plume 250
Towards New Hypergolic Hydrogen Peroxide-Based Bipropellants 248
Effects of Different Nano-Sized Metal Oxide Catalysts on the Properties of Composite Solid Propellants 239
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 235
Evaluation of a Ramjet Model in a Supersonic High-Enthalpy Tunnel 235
Hybrid Combustion Studies on Regression Rate Enhancement and Transient Ballistic Response 234
Free and Forced Oscillations of Magnetic Liquids Under Low-Gravity Conditions 233
Detailed Properties of Iron Oxide Solid Propellant Catalyst 231
Active Debris Multi-Removal Mission Concept Based on Hybrid Propulsion 229
Combustion of Metal Agglomerates in a Solid Rocket Core Flow 228
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 228
Fragmentation of Ammonium Nitrate Particles under Thermal Cycling 227
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 227
Active Space Debris Removal by a Hybrid Propulsion Module 225
Experimental techniques for characterization of particles in plumes of sub-scale solid rocket motors 225
A Two-Phase Mass Flow Rate Model for Nitrous Oxide Based on Void Fraction 225
Activated and Nano-Sized Aluminum as Metal Fuels in Solid Rocket Propellants 221
Role of Pressure and Aluminum Size in Solid Propellant CCP Generation 219
Parallel packing code for propellant microstructure analysis 219
Trade-Off Analysis of a New Liquid Rocket Engine 216
Prospects of Aluminum Modifications as Energetic Fuels in Chemical Rocket Propulsion 215
Overview of Additive Manufacturing and Quality Assurance of Powders for Space Propulsive Components 212
Burning Rate Measurements on Damaged Propellant Samples Under Mechanical Loads 208
Numerical Simulation of HTPB Combustion in a 2D Hybrid Slab Combustor 206
Thermite-For-Demise (T4D): Material Selection for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 204
Aggregation Versus Agglomeration in Metallized Solid Rocket Propellants 204
Collecting Data on Aluminum Combustion and Its Oxides in Solid Rocket Motors 204
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 202
Preliminary Assessments for the Development of a Green Storable Bipropellant Rocket Engine Based on H2O2 202
Efficient Solid Rocket Propulsion for Access to Space 201
Diagnostics for Entrainment Characterization in Liquefying Fuel Formulations 200
Burn-Rate Measurement on Small-Scale Rocket Motors 199
2D Numerical Simulation of Combustion Processes in a Slab Hybrid Rocket Motor 199
Burning Behavior of ADN-Based Propellants Loaded with Al-Mg Mechanically Activated Powders 199
Microstructure Effects in Aluminized Solid Rocket Propellants 198
Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems 198
Burning Rate Modifiers to Tailor Combustion of ADN/AN-Based Solid Propellants 198
Thermite-for-Demise (T4D): Experimental analysis of heat transfer principles and preliminary sizing of an application 195
Time-resolved burning of solid fuels for hybrid rocket propulsion 195
Monte Carlo Uncertainty Quantification Using Quasi-1D SRM Ballistic Model 194
Aging Effects on Nano-Sized Aluminum Reactivity 193
Thermite-for-demise (T4D): Experiments and numerical modelling on ball-bearing unit mock-ups containing thermite in an arc-heated wind tunnel 190
Particulate Phase Evolution Inside Solid Rocket Motors: Preliminary Results 190
Aluminized Gels or Clouds for Low Trust Applications 189
Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion 187
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 187
Combustion of Metal Agglomerates in Solid Rocket Core Flow 186
Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Conceptual and Detailed Design 186
Photo-polymerization for additive manufacturing of composite solid propellants 186
Environmental impact of propulsion systems and green alternatives 185
Quantification of HCl in Solid Propellant Combustion Products 185
Agglomeration of Aluminized Solid Rocket Propellants 184
Combustion in a Lab-Scale Vortex Flow Hybrid Rocket Engine 184
Overview of a supersonic probe for solid propellant rocket CCP collection 183
Monoethanolamine-Based Fuels Hypergolic with Rocket-Grade Hydrogen Peroxide 181
Solid Rocket Propellant Photo-Polymerization with an In-House LED-UV Prototype 180
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 179
Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Application of Quasi-1D Engineering Model and 2D Axisymmetric CFD 179
Active Space Debris Removal by Hybrid Engine Module 178
Mechanical Characterization of Composite Solid Propellants 177
Agglomeration and Pocket Structures in Composite Solid Rocket Propellants 177
Innovative Metallized Formulations for Solid or Hybrid Rocket Propulsion 177
Pocket Model for Aluminum Agglomeration Based on Propellant Microstructure 174
Ignition of Mechanically Activated Aluminum Powders Doped with Metal Oxides 173
Thermite-for-Demise (T4D): Preliminary Assessment on the Effects of a Thermite Charge in Arc-Heated Wind Tunnel Experiments 171
An Hybrid Microcombustor for Regression Rate Measurements 171
Agglomeration in Solid Rocket Propellants: Novel Experimental and Modeling Methods 171
Monte Carlo Analysis of a LEO Reentry Mission by Solid Rocket Propulsion 171
Thermite-for-Demise: Preliminary on-Ground Heat Transfer Experimental Testing 170
Experimental Characterization of Al/Mg Dual Metal Neutralizing Propellants 170
Thermite-for-demise (T4D): experiments and numerical modelling on solar array drive mechanism mock-ups containing thermite in an arc-heated wind tunnel 170
Advanced Aluminum Powders for Solid Propellants 169
Experimental and Numerical Investigation of the Condensed Combustion Products of AP-based Rocket Propellants 168
Innovative Metal Fuels for Solid Rocket Propulsion 166
Simulation Code for Hybrid Rocket Combustion 165
Activation of Micrometric Aluminum - Metal Oxide Mixtures by Mechanical Milling 165
Thermal behavior and decomposition kinetics of composite solid propellants in the presence of amide burning rate suppressants 165
Current Environmental Concerns About Space and Suborbital Launch Activities 165
Intrinsic Structural-Ballistic Interactions in Composite Energetic Materials. Part I: Experiments 164
An Experimental Assessment of Soil Contamination by Composite Solid Rocket Propellants 163
Caratterizzazione meccanica e applicazione di modelli iperelastici ad un materiale plastico a base di legante per uso propulsivo spaziale 163
Grain Processing Effects on Steady Burning Rate in Small Scale Test Motors 162
Novel Activated Metal Powders for Improved Hybrid Fuels and Green Solid Propellants 162
Curing Viscosity of HTPB-Based Binder Embedding Micro and Nano-Aluminum Particles 161
Hydrogen-Based Thrusters for Supersonic and Hypersonic Flight: Experimental Characterization 160
Totale 20.854
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Categoria #
all - tutte 92.404
article - articoli 27.966
book - libri 0
conference - conferenze 58.031
curatela - curatele 0
other - altro 0
patent - brevetti 1.894
selected - selezionate 0
volume - volumi 4.513
Totale 184.808
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021787 0 0 0 0 0 0 0 0 0 179 161 447
2021/20221.866 115 211 222 76 225 102 120 135 58 118 174 310
2022/20232.515 325 227 84 176 238 251 40 165 363 346 165 135
2023/20241.586 92 195 84 158 87 190 256 79 50 163 79 153
2024/20256.366 318 96 194 280 1.094 372 224 574 743 290 684 1.497
2025/202616.027 3.718 2.607 937 1.129 875 939 2.397 1.053 956 1.416 0 0
Totale 37.680