GALFETTI, LUCIANO
 Distribuzione geografica
Continente #
NA - Nord America 16.169
EU - Europa 12.649
AS - Asia 7.120
SA - Sud America 1.219
AF - Africa 383
Continente sconosciuto - Info sul continente non disponibili 222
OC - Oceania 55
Totale 37.817
Nazione #
US - Stati Uniti d'America 15.678
RU - Federazione Russa 4.290
IT - Italia 4.149
CN - Cina 2.039
SG - Singapore 1.994
VN - Vietnam 1.065
BR - Brasile 1.038
UA - Ucraina 614
DE - Germania 612
FR - Francia 542
SE - Svezia 539
KR - Corea 431
FI - Finlandia 385
GB - Regno Unito 364
CA - Canada 352
IN - India 307
ES - Italia 253
JP - Giappone 219
IE - Irlanda 208
NL - Olanda 179
AT - Austria 153
MA - Marocco 145
HK - Hong Kong 134
TR - Turchia 123
JO - Giordania 115
CI - Costa d'Avorio 107
CH - Svizzera 93
ID - Indonesia 83
BD - Bangladesh 82
PH - Filippine 80
BE - Belgio 76
PL - Polonia 75
IR - Iran 66
TW - Taiwan 66
MX - Messico 59
AR - Argentina 58
IQ - Iraq 47
PK - Pakistan 44
ZA - Sudafrica 40
EC - Ecuador 33
AU - Australia 30
AE - Emirati Arabi Uniti 29
SA - Arabia Saudita 28
NZ - Nuova Zelanda 25
CO - Colombia 24
MY - Malesia 24
GR - Grecia 23
KZ - Kazakistan 21
TH - Thailandia 21
IL - Israele 19
KE - Kenya 19
DZ - Algeria 17
EG - Egitto 17
VE - Venezuela 17
CL - Cile 15
UZ - Uzbekistan 15
PT - Portogallo 14
CR - Costa Rica 13
JM - Giamaica 13
PY - Paraguay 13
TT - Trinidad e Tobago 12
RO - Romania 11
AZ - Azerbaigian 10
DO - Repubblica Dominicana 10
HU - Ungheria 10
NP - Nepal 10
TN - Tunisia 9
BO - Bolivia 8
CZ - Repubblica Ceca 8
LT - Lituania 8
BG - Bulgaria 7
NG - Nigeria 7
PE - Perù 7
HN - Honduras 6
OM - Oman 6
AL - Albania 5
DK - Danimarca 5
EU - Europa 5
LV - Lettonia 5
SV - El Salvador 5
SY - Repubblica araba siriana 5
UY - Uruguay 5
ET - Etiopia 4
GT - Guatemala 4
KG - Kirghizistan 4
MU - Mauritius 4
QA - Qatar 4
RS - Serbia 4
AO - Angola 3
BB - Barbados 3
BH - Bahrain 3
BZ - Belize 3
EE - Estonia 3
GE - Georgia 3
LB - Libano 3
LK - Sri Lanka 3
NI - Nicaragua 3
PS - Palestinian Territory 3
SN - Senegal 3
BA - Bosnia-Erzegovina 2
Totale 37.557
Città #
Ashburn 1.913
Milan 1.379
San Jose 1.294
Singapore 1.082
Fairfield 992
Woodbridge 954
Chandler 831
Wilmington 641
Santa Clara 627
Houston 595
Ann Arbor 577
Moscow 564
Council Bluffs 527
Seattle 439
Boardman 386
Cambridge 365
Jacksonville 354
Beijing 352
Hefei 346
Seoul 334
The Dalles 332
Dallas 312
Dearborn 254
Lawrence 226
Dong Ket 225
Medford 223
Ottawa 215
Málaga 207
Lauterbourg 201
Dublin 200
Ho Chi Minh City 199
Rome 195
Los Angeles 191
Helsinki 186
Tokyo 183
North Charleston 161
Hanoi 160
Vienna 136
New York 132
Redwood City 126
Buffalo 117
Amman 114
Abidjan 107
Hong Kong 100
Kenitra 92
São Paulo 76
Shanghai 74
Des Moines 71
Bern 68
Frankfurt am Main 68
Orem 67
Marnate 65
Bovisio Masciago 63
Segrate 62
Redmond 59
Jakarta 58
Brussels 57
Ciampino 56
Taipei 53
Guangzhou 51
Amsterdam 50
Mumbai 50
Warsaw 49
Chicago 47
Davao City 47
San Diego 47
Las Vegas 46
Phoenix 46
Istanbul 40
Zhengzhou 40
Monza 39
Norwalk 38
Washington 38
Casablanca 37
Chennai 37
Da Nang 36
London 36
Nanjing 34
Turin 34
Denver 33
Stockholm 33
Basingstoke 31
Giussano 31
Hangzhou 31
Montreal 31
Naples 31
Rio de Janeiro 29
Toronto 29
Rho 28
Brooklyn 27
Changsha 27
Mountain View 26
Belo Horizonte 24
Bologna 24
Atlanta 23
West Lafayette 23
Xian 23
Gavirate 22
Johannesburg 22
Palermo 22
Totale 21.455
Nome #
Advanced Hybrid Solid Fuels 450
Accelerated ageing of micron- and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity 350
Aluminum powders: aging effects on metal content and thermogravimetry reactivity 318
A Critical Analysis of Paraffin-based Fuel Formulations for Hybrid Rocket Propulsion 316
Combustion Processes in Hybrid Rockets 306
A method for mechanical activation of powders by means of balls 302
Experimental investigation of paraffin-based fuels for hybrid rocket propulsion 300
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 297
Aerospace Propulsion Research Activities at SPlab. Overview and Results 293
Iron oxide as solid propellant catalyst: A detailed characterization 289
Paraffin-Based Fuels and Energetic Additives for Hybrid Rocket Propulsion 282
Preliminary kinetic characterization of lithium-aluminum based hydrides for airbreathing propulsion 280
Macro- vs Microcrystalline Wax: Interplay of Evaporation and Decomposition under Pressure Variation 278
Burning Behavior Investigation of a Vortex Flow Pancake Hybrid Rocket Engine 278
Paraffin-based Solid Fuels for Hybrid Propulsion Filled with Lithium Aluminum Hydride: Thermal, Mechanical and Ballistic Characterization 277
Green Fuels for Rocket Propulsion: Current Status and Future Perspectives of Paraffin-Based Formulations 272
Experimental evaluation of HTPB/paraffin fuel blends for hybrid rocket applications 271
Experimental data from ramjet/scramjet combustion and numerical validation perspectives 269
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part I, Mechanical and Pre-Burning Characterization 265
Development of an intrusive technique for particles collection in rockets plume 264
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Mechanical characterization 264
Aluminum Particle Size Influence on Ignition and Combustion of AP/HTPB/Al Solid Rocket Propellants 258
Evaluation of a Ramjet Model in a Supersonic High-Enthalpy Tunnel 255
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 244
Detailed Properties of Iron Oxide Solid Propellant Catalyst 242
Hybrid Combustion Studies on Regression Rate Enhancement and Transient Ballistic Response 242
A Wide Characterization of Paraffin-based Fuels Mixed with Styrene-based Thermoplastic Polymers for Hybrid Propulsion 240
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 240
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 240
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 238
Thermite-For-Demise (T4D): Material Selection for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 237
Activated and Nano-Sized Aluminum as Metal Fuels in Solid Rocket Propellants 232
Influence of Operating Parameters on the Ballistics of a Lab-Scale Vortex Flow Pancake Hybrid Rocket Engine 232
Role of Pressure and Aluminum Size in Solid Propellant CCP Generation 231
A Parametric Study of the Effect of Liquid Fuel Entrainment on the Combustion Characteristics of a Paraffin-Based Hybrid Rocket Motor 230
Nano-Aluminum as Energetic Material for Rocket Propellants 228
Trade-Off Analysis of a New Liquid Rocket Engine 227
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part II, Ballistic Characterization 219
Microstructure Effects in Aluminized Solid Rocket Propellants 215
Numerical Simulation of HTPB Combustion in a 2D Hybrid Slab Combustor 215
Efficient Solid Rocket Propulsion for Access to Space 212
Regression Rate and Combustion Efficiency in a Vortex-Flow Hybrid Rocket Engine 212
Diagnostics for Entrainment Characterization in Liquefying Fuel Formulations 210
Towards High-Performing Paraffin-Based Fuels Exploiting the Armored Grain Concept 209
An Italian Network to Improve Hybrid Rocket Performance: Strategy and Results 208
2D Numerical Simulation of Combustion Processes in a Slab Hybrid Rocket Motor 206
Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems 206
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 205
Physical and Ballistic Characterization of AlH3-Based Space Propellants 202
Aging Effects on Nano-Sized Aluminum Reactivity 202
Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Conceptual and Detailed Design 201
Time-resolved burning of solid fuels for hybrid rocket propulsion 200
Experimental Investigation of Solid Fuels for Hybrid Rocket Propulsion 200
Combustion in a Lab-Scale Vortex Flow Hybrid Rocket Engine 198
Pre and Post-Burning Analysis of Nano-Aluminized Solid Rocket Propellants 198
Experimental Investigations on Transient Burning of Nano-Aluminized Solid Rocket Propellants 197
Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion 196
A Wide Characterization of Aluminum Powders for Propellants 195
Innovative Metallized Formulations for Solid or Hybrid Rocket Propulsion 195
An experimental investigation of convective heat transfer at evaporation of kerosene and water in the closed volume 195
Overview of a supersonic probe for solid propellant rocket CCP collection 195
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 195
Aging of ADN Rocket Propellant Formulations with Desmophen-Based Elastomer Binder 193
Development of Paraffin-Based Fuels for a Vortex Combustion Hybrid Rocket Engine 192
Flame Surface Modification of Polyethylene Sheets 192
Paraffin-Based Fuels For Hybrid Propulsion: Characterization Of Waxes And Its Blends 192
Characterization of ADN/GAP-Based and ADN/Desmophen-Based Propellant Formulations and Comparison with AP Analogues 191
Mechanical Characterization of Composite Solid Propellants 190
Actualization of an efficient throttleable laser propulsion mode 190
Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Application of Quasi-1D Engineering Model and 2D Axisymmetric CFD 189
Experimental Investigation of the Condensed Combustion Products of Micro Aluminized Solid Rocket Propellants 188
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 187
A Global Characterization of Nano-Aluminized Propellants 186
Experimental Investigation and Numerical Modeling of the Condensed Combustion Products of Micro and Nano-Aluminized Solid Propellants 185
Pure Paraffin Waxes Analysis for Hybrid Rocket Solid Fuels: Rheological, Thermal and Mechanical Characterization 184
Impact of 3d-printing on the mechanical reinforcement and the ballistic response of paraffin-based fuels: The armored grain 184
Aging of HTPB/Al/AP Rocket Propellant Formulations Investigated by DMA Measurements 182
Hydrogen Generation from Aluminum Composites Hydrolysis for Space Propulsion 181
Paraffin-Based Solid Fuels for Hybrid Propulsion Filled with Lithium Aluminum Hydride: Thermal, Mechanical and Ballistic Characterization 181
Nano-Composites for Rocket Solid Propellants 181
Ageing of HTPB/Al/AP Rocket Propellant Formulations Investigated by DMA Measurements, Sol-Gel and GPC Analysis 179
Particle Size in SRM Plume: Assessment of Collection Method 179
An Hybrid Microcombustor for Regression Rate Measurements 178
Experimental and Numerical Investigation of the Condensed Combustion Products of AP-based Rocket Propellants 178
Novel Activated Metal Powders for Improved Hybrid Fuels and Green Solid Propellants 178
Experimental Visualizations of Entrainment Phenomena in Wax-Based Fuels for Hybrid Space Propulsion 177
Flame Surface Modification of Polyethylene Sheets 176
Advanced Hybrid Propellant for a Moon Orbiter Thruster 176
Nanoaluminum as a Solid Propellant Fuel 176
Effect of mechanical activation on the reactivity of composites for flameless heaters 175
Vortex combustion in a hybrid rocket motor 174
Thermite-for-Demise (T4D): Concept Definition for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 174
Reduction of Solid Propellants Environmental Impact: Al-Mg Mechanically Activated Fuels and AP-PSAN Blends 173
Hydrogen-Based Thrusters for Supersonic and Hypersonic Flight: Experimental Characterization 171
Active De-Orbiting Systems of Launcher Upper Stages and Spacecraft Based on Hybrid Gas Rocket Engines 170
Ageing Behaviour of Composite Rocket Propellant Formulations Investigated by DMA, SGA, and GPC 170
Simulation Code for Hybrid Rocket Combustion 169
Ballistics and Condensed Residues of Aluminized Solid Rocket Propellants 168
Characterization of a Family of Paraffin-Based Solid Fuels 168
Theoretical Analysis of Hydrides in Solid and Hybrid Rocket Propulsion 167
Totale 21.967
Categoria #
all - tutte 99.873
article - articoli 19.381
book - libri 0
conference - conferenze 73.664
curatela - curatele 682
other - altro 0
patent - brevetti 1.359
selected - selezionate 0
volume - volumi 4.787
Totale 199.746


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20221.962 0 249 131 107 322 118 126 139 74 137 196 363
2022/20232.627 348 257 120 164 244 258 45 170 394 285 155 187
2023/20241.415 92 214 63 125 103 218 154 78 24 129 59 156
2024/20254.758 112 102 156 118 984 275 169 463 598 256 635 890
2025/202614.868 2.850 2.417 780 957 707 776 2.108 821 670 1.367 362 1.053
2026/2027708 401 307 0 0 0 0 0 0 0 0 0 0
Totale 37.817