GALFETTI, LUCIANO
 Distribuzione geografica
Continente #
EU - Europa 2.465
AS - Asia 1.284
NA - Nord America 983
AF - Africa 84
SA - Sud America 81
OC - Oceania 51
Continente sconosciuto - Info sul continente non disponibili 1
Totale 4.949
Nazione #
IT - Italia 1.526
US - Stati Uniti d'America 918
IN - India 258
CN - Cina 229
FR - Francia 202
GB - Regno Unito 131
TR - Turchia 131
DE - Germania 120
JP - Giappone 97
KR - Corea 96
IR - Iran 85
NL - Olanda 84
RU - Federazione Russa 70
PL - Polonia 66
VN - Vietnam 66
CA - Canada 49
SG - Singapore 48
BR - Brasile 46
AU - Australia 44
MY - Malesia 37
SE - Svezia 34
EG - Egitto 32
HK - Hong Kong 32
IL - Israele 32
TW - Taiwan 32
CZ - Repubblica Ceca 29
PK - Pakistan 28
BE - Belgio 27
ES - Italia 24
ID - Indonesia 21
PT - Portogallo 21
UA - Ucraina 20
TH - Thailandia 17
BD - Bangladesh 16
DZ - Algeria 16
ET - Etiopia 15
MX - Messico 14
RS - Serbia 14
RO - Romania 13
HU - Ungheria 12
LB - Libano 12
FI - Finlandia 11
CH - Svizzera 10
DK - Danimarca 10
CL - Cile 9
CO - Colombia 9
AE - Emirati Arabi Uniti 8
AR - Argentina 8
AT - Austria 8
ZA - Sudafrica 8
KZ - Kazakistan 7
IQ - Iraq 6
YE - Yemen 6
NO - Norvegia 5
AM - Armenia 4
BA - Bosnia-Erzegovina 4
BO - Bolivia 4
IE - Irlanda 4
NP - Nepal 4
NZ - Nuova Zelanda 4
SA - Arabia Saudita 4
SK - Slovacchia (Repubblica Slovacca) 4
GR - Grecia 3
LT - Lituania 3
MP - Marianne Settentrionali, isole 3
SI - Slovenia 3
TN - Tunisia 3
ZW - Zimbabwe 3
ER - Eritrea 2
LV - Lettonia 2
NG - Nigeria 2
PH - Filippine 2
PY - Paraguay 2
SY - Repubblica araba siriana 2
VE - Venezuela 2
BG - Bulgaria 1
BJ - Benin 1
BN - Brunei Darussalam 1
CI - Costa d'Avorio 1
CU - Cuba 1
EC - Ecuador 1
EE - Estonia 1
EU - Europa 1
HN - Honduras 1
HR - Croazia 1
IS - Islanda 1
JO - Giordania 1
KG - Kirghizistan 1
LU - Lussemburgo 1
MA - Marocco 1
MO - Macao, regione amministrativa speciale della Cina 1
Totale 4.949
Città #
Milan 320
Rome 74
Turin 60
Ashburn 54
Houston 40
Istanbul 39
Beijing 38
Ankara 37
Seoul 36
Paris 34
Amsterdam 32
Fairfield 30
Segrate 29
West Lafayette 28
Council Bluffs 27
Hanoi 26
Hyderabad 26
Boardman 25
Fremont 25
Trezzano Sul Naviglio 25
Dong Ket 24
Redmond 24
Seattle 24
Ann Arbor 23
Bengaluru 23
Mumbai 23
Woodbridge 21
Chennai 20
Santa Cruz 20
Buffalo 18
Chicago 18
Kuala Lumpur 18
Toulouse 18
Brasília 17
Changsha 17
Dallas 16
Erba 16
Helwan 16
Jinan 16
Cambridge 15
London 15
Tokyo 15
Wilmington 15
Los Angeles 14
Mountain View 14
New York 14
Toronto 14
Atatürk 13
Delhi 13
Hangzhou 13
Parma 13
Taipei 13
Warsaw 13
Naples 12
Central 11
Guangzhou 11
Monza 11
Roncello 11
Shenyang 11
Stockholm 11
Bangkok 10
Bovisio Masciago 10
Brussels 10
College Station 10
Dhaka 10
Fleming Island 10
Haifa 10
Jakarta 10
Pune 10
San Antonio 10
San Giuliano Milanese 10
San Jose 10
Wuhan 10
Xi'an 10
Belgrade 9
Bologna 9
Como 9
Frankfurt am Main 9
Hsinchu 9
Islamabad 9
Kochi 9
Marnate 9
Nanjing 9
Bathinda 8
Columbus 8
Delft 8
Lisbon 8
Lodz 8
Melbourne 8
Munich 8
Polska 8
Reggio Emilia 8
Rozzano 8
Sharqia 8
Sydney 8
Tehran 8
Bursa 7
Columbia 7
Coral Gables 7
Desio 7
Totale 2.002
Nome #
Trade-Off Analysis of a New Liquid Rocket Engine, file e0c31c0d-d886-4599-e053-1705fe0aef77 768
Combustion Processes in Hybrid Rockets, file e0c31c0e-8c43-4599-e053-1705fe0aef77 388
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part I, Mechanical and Pre-Burning Characterization, file e0c31c0d-c1e9-4599-e053-1705fe0aef77 257
An Italian Network to Improve Hybrid Rocket Performance: Strategy and Results, file e0c31c0e-7465-4599-e053-1705fe0aef77 204
Aging of ADN Rocket Propellant Formulations with Desmophen-Based Elastomer Binder, file e0c31c0e-b97d-4599-e053-1705fe0aef77 188
Mechanically Activated Al/Mg Powders for Solid Rocket Propellants, file e0c31c0d-bfc8-4599-e053-1705fe0aef77 170
Characterization of ADN/GAP-Based and ADN/Desmophen-Based Propellant Formulations and Comparison with AP Analogues, file e0c31c0e-746a-4599-e053-1705fe0aef77 163
A Wide Characterization of Paraffin-based Fuels Mixed with Styrene-based Thermoplastic Polymers for Hybrid Propulsion, file e0c31c08-0e6e-4599-e053-1705fe0aef77 159
Thermite-for-Demise (T4D): Concept Definition for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry, file 240c430c-007f-44cb-9af3-f74ad4663713 155
Influence of Operating Parameters on the Ballistics of a Lab-Scale Vortex Flow Pancake Hybrid Rocket Engine, file e0c31c0e-2922-4599-e053-1705fe0aef77 145
Macro- vs Microcrystalline Wax: Interplay of Evaporation and Decomposition under Pressure Variation, file e0c31c0f-7168-4599-e053-1705fe0aef77 137
Activated and Nano-Sized Aluminum as Metal Fuels in Solid Rocket Propellants, file e0c31c0d-bfca-4599-e053-1705fe0aef77 136
Accelerated ageing of micron- and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity, file e0c31c0c-d1c7-4599-e053-1705fe0aef77 127
An experimental investigation of convective heat transfer at evaporation of kerosene and water in the closed volume, file e0c31c0e-3e74-4599-e053-1705fe0aef77 127
Catalyst Screening for Ammonium Nitrate Oxidizer, file e0c31c0b-37a8-4599-e053-1705fe0aef77 117
Evaluation of a Ramjet Model in a Supersonic High-Enthalpy Tunnel, file e0c31c0e-71fc-4599-e053-1705fe0aef77 107
Effect of mechanical activation on the reactivity of composites for flameless heaters, file e0c31c10-0f29-4599-e053-1705fe0aef77 105
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Mechanical characterization, file e0c31c11-014f-4599-e053-1705fe0aef77 103
Development of an intrusive technique for particles collection in rockets plume, file e0c31c0c-d1b8-4599-e053-1705fe0aef77 102
Iron oxide as solid propellant catalyst: A detailed characterization, file e0c31c0e-ac62-4599-e053-1705fe0aef77 101
Numerical and Experimental Investigation of a Lab-Scale Paraffin Motor with Swirled Injection of Gaseous Oxygen, file e46d01ea-178e-489c-9b2d-4d9ec6eef619 99
Particle Size in SRM Plume: Assessment of Collection Method, file e0c31c0d-bfcf-4599-e053-1705fe0aef77 97
Reduction of Solid Propellants Environmental Impact: Al-Mg Mechanically Activated Fuels and AP-PSAN Blends, file 4c4fbae4-7880-4e62-8437-61946c5921c5 91
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part II, Ballistic Characterization, file e0c31c0e-567f-4599-e053-1705fe0aef77 90
Aluminum powders: aging effects on metal content and thermogravimetry reactivity, file e0c31c0d-3fd9-4599-e053-1705fe0aef77 82
Experimental evaluation of HTPB/paraffin fuel blends for hybrid rocket applications, file e0c31c10-8fe8-4599-e053-1705fe0aef77 79
Towards High-Performing Paraffin-Based Fuels Exploiting the Armored Grain Concept, file 6def32d2-ec17-4117-9bd4-9aeffef7a538 72
Detailed Properties of Iron Oxide Solid Propellant Catalyst, file e0c31c0b-369d-4599-e053-1705fe0aef77 70
Space Debris Mitigation and Remediation: Perspectives of Affordable Hybrid Propulsion Implementations, file e0c31c0c-138a-4599-e053-1705fe0aef77 68
Role of Pressure and Aluminum Size in Solid Propellant CCP Generation, file e0c31c0b-39d8-4599-e053-1705fe0aef77 65
Development of Paraffin-Based Fuels for a Vortex Combustion Hybrid Rocket Engine, file 3c602eae-a011-41b0-a493-a218d99030b3 59
A method for mechanical activation of powders by means of balls, file e0c31c0f-575c-4599-e053-1705fe0aef77 56
Paraffin-based Solid Fuels for Hybrid Propulsion Filled with Lithium Aluminum Hydride: Thermal, Mechanical and Ballistic Characterization, file e0c31c0e-50e6-4599-e053-1705fe0aef77 55
Preliminary kinetic characterization of lithium-aluminum based hydrides for airbreathing propulsion, file e0c31c0e-0000-4599-e053-1705fe0aef77 51
A wide characterization of Paraffin-based Fuels Mixed with Styrene-based thermoplastic polymers for hybrid propulsion, file e0c31c11-095a-4599-e053-1705fe0aef77 37
Hydrogen Generation from Aluminum Composites Hydrolysis for Space Propulsion, file f607dc1e-b4ec-4893-96a6-4fad6a54ed9c 36
Aerospace Propulsion Research Activities at SPlab. Overview and Results, file e0c31c0e-6baf-4599-e053-1705fe0aef77 13
Preliminary kinetic characterization of lithium-aluminum based hydrides for airbreathing propulsion, file e0c31c0b-8c2a-4599-e053-1705fe0aef77 10
Iron oxide as solid propellant catalyst: A detailed characterization, file e0c31c0c-cff5-4599-e053-1705fe0aef77 10
Macro- vs Microcrystalline Wax: Interplay of Evaporation and Decomposition under Pressure Variation, file e0c31c0b-2fda-4599-e053-1705fe0aef77 8
Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems, file e0c31c09-3473-4599-e053-1705fe0aef77 7
A Critical Analysis of Paraffin-based Fuel Formulations for Hybrid Rocket Propulsion, file e0c31c0b-3b3c-4599-e053-1705fe0aef77 7
Green Fuels for Rocket Propulsion: Current Status and Future Perspectives of Paraffin-Based Formulations, file e0c31c0e-7202-4599-e053-1705fe0aef77 7
An experimental investigation of convective heat transfer at evaporation of kerosene and water in the closed volume, file e0c31c0b-95d4-4599-e053-1705fe0aef77 6
Regression Rate and Combustion Efficiency in a Vortex-Flow Hybrid Rocket Engine, file e0c31c0e-69e2-4599-e053-1705fe0aef77 6
Characterization of ADN/GAP-Based and ADN/Desmophen-Based Propellant Formulations and Comparison with AP Analogues, file e0c31c08-1697-4599-e053-1705fe0aef77 5
Aging of ADN Rocket Propellant Formulations with Desmophen-Based Elastomer Binder, file e0c31c08-1d5f-4599-e053-1705fe0aef77 5
Paraffin-based Solid Fuels for Hybrid Propulsion Filled with Lithium Aluminum Hydride: Thermal, Mechanical and Ballistic Characterization, file e0c31c0b-2c46-4599-e053-1705fe0aef77 5
Aging Effects on Nano-Sized Aluminum Reactivity, file e0c31c0b-3e7e-4599-e053-1705fe0aef77 5
Hybrid Combustion Studies on Regression Rate Enhancement and Transient Ballistic Response, file e0c31c0e-1acb-4599-e053-1705fe0aef77 5
An Italian Network to Improve Hybrid Rocket Performance: Strategy and Results, file e0c31c08-1e87-4599-e053-1705fe0aef77 4
Paraffin-Based Fuels For Hybrid Propulsion: Characterization Of Waxes And Its Blends, file e0c31c0a-325a-4599-e053-1705fe0aef77 3
Development of a Compact Hybrid Rocket Engine for Low-Cost In-Space Propulsion, file e0c31c0d-74c3-4599-e053-1705fe0aef77 3
Experimental data from ramjet/scramjet combustion and numerical validation perspectives, file e0c31c0e-1f5c-4599-e053-1705fe0aef77 3
Thermite-For-Demise (T4D): Material Selection for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry, file 685dec27-3def-4895-a081-e70f502309fe 2
End-To-end Flight Test for Planetary Landing, an Unprecedented Approach in Europe, file e0c31c08-0cc4-4599-e053-1705fe0aef77 2
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution, file e0c31c08-7e86-4599-e053-1705fe0aef77 2
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion, file e0c31c09-3d68-4599-e053-1705fe0aef77 2
Effects of Aluminum Composites on the Regression Rates of Solid Fuels, file e0c31c09-86cd-4599-e053-1705fe0aef77 2
Paraffin-Based Solid Fuels Characterization and Effect of Their Properties on Entrainment Phenomena, file e0c31c09-86cf-4599-e053-1705fe0aef77 2
Combustion Properties of Aluminum-Based Oxidizer-Lean Propellants, file e0c31c0b-33bf-4599-e053-1705fe0aef77 2
Quasi-steady and Forced Transient Burning of a Vortex Flow Hybrid Motor, file e0c31c0b-369c-4599-e053-1705fe0aef77 2
Combustion in a Lab-Scale Vortex Flow Hybrid Rocket Engine, file e0c31c0b-99fc-4599-e053-1705fe0aef77 2
Accelerated ageing of micron- and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity, file e0c31c0c-dca5-4599-e053-1705fe0aef77 2
Overview of a supersonic probe for solid propellant rocket CCP collection, file e0c31c0d-3c49-4599-e053-1705fe0aef77 2
Combustion Processes in Hybrid Rockets, file e0c31c0e-8ddf-4599-e053-1705fe0aef77 2
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Mechanical characterization, file e0c31c10-000f-4599-e053-1705fe0aef77 2
Impact of 3d-printing on the mechanical reinforcement and the ballistic response of paraffin-based fuels: The armored grain, file e0c31c10-56c3-4599-e053-1705fe0aef77 2
Rheological and Mechanical Characterization of Hybrid Rocket Solid Fuels, file e0c31c07-e22f-4599-e053-1705fe0aef77 1
Aging of HTPB/Al/AP Rocket Propellant Formulations Investigated by DMA Measurements, file e0c31c08-1002-4599-e053-1705fe0aef77 1
Paraffin-Based Fuels and Energetic Additives for Hybrid Rocket Propulsion, file e0c31c08-6fc3-4599-e053-1705fe0aef77 1
Theoretical Analysis of Hydrides in Solid and Hybrid Rocket Propulsion, file e0c31c08-7798-4599-e053-1705fe0aef77 1
Innovative Metallized Formulations for Solid or Hybrid Rocket Propulsion, file e0c31c08-7c9b-4599-e053-1705fe0aef77 1
Uncertainty Propagation in Post-Firing Analysis of SRM Internal Ballistics, file e0c31c09-3475-4599-e053-1705fe0aef77 1
A Parametric Study of the Effect of Liquid Fuel Entrainment on the Combustion Characteristics of a Paraffin-Based Hybrid Rocket Motor, file e0c31c09-86cc-4599-e053-1705fe0aef77 1
Experimental Visualizations of Entrainment Phenomena in Wax-Based Fuels for Hybrid Space Propulsion, file e0c31c09-86d1-4599-e053-1705fe0aef77 1
Experimental Investigation of Solid Fuels for Hybrid Rocket Propulsion, file e0c31c09-86d3-4599-e053-1705fe0aef77 1
Paraffin-Based Solid Fuels for Hybrid Propulsion Filled with Lithium Aluminum Hydride: Thermal, Mechanical and Ballistic Characterization, file e0c31c09-94d1-4599-e053-1705fe0aef77 1
Vortex combustion in a hybrid rocket motor, file e0c31c09-e25e-4599-e053-1705fe0aef77 1
Isothermal Two-Fluid Based CFD of Solid-Liquid Slush Flows for Propulsion Systems, file e0c31c0a-ec2f-4599-e053-1705fe0aef77 1
Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Conceptual and Detailed Design, file e0c31c0b-33c0-4599-e053-1705fe0aef77 1
Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Application of Quasi-1D Engineering Model and 2D Axisymmetric CFD, file e0c31c0b-3462-4599-e053-1705fe0aef77 1
Numerical Simulation of Vortex Combustion in a Hybrid Rocket Motor, file e0c31c0b-3e80-4599-e053-1705fe0aef77 1
Development of an intrusive technique for particles collection in rockets plume, file e0c31c0c-d1b7-4599-e053-1705fe0aef77 1
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion, file e0c31c0d-ae3c-4599-e053-1705fe0aef77 1
Performance and Environmental Impact Prediction of SRMs. Road Map for Reliable Dataset of Particles in Plume, file e0c31c0e-715a-4599-e053-1705fe0aef77 1
Particle Size in Solid Rocket Motor Plume: New Experimental Method, file e0c31c0e-89e2-4599-e053-1705fe0aef77 1
Experimental evaluation of HTPB/paraffin fuel blends for hybrid rocket applications, file e0c31c10-9643-4599-e053-1705fe0aef77 1
Actualization of an efficient throttleable laser propulsion mode, file e0c31c11-31e5-4599-e053-1705fe0aef77 1
Totale 5.027
Categoria #
all - tutte 9.890
article - articoli 4.839
book - libri 0
conference - conferenze 4.876
curatela - curatele 0
other - altro 0
patent - brevetti 163
selected - selezionate 0
volume - volumi 12
Totale 19.780


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/201947 0 0 0 0 0 0 0 0 2 4 15 26
2019/2020357 22 14 33 45 32 29 12 28 19 32 56 35
2020/2021785 34 38 46 61 74 64 65 81 82 74 76 90
2021/20221.020 85 95 79 76 81 76 85 85 76 91 108 83
2022/20231.467 73 72 110 142 114 135 100 189 144 162 123 103
2023/20241.261 113 152 133 164 117 125 182 157 118 0 0 0
Totale 5.027