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

PARAVAN, CHRISTIAN
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
EU - Europa 8.861
NA - Nord America 7.748
AS - Asia 4.256
SA - Sud America 757
AF - Africa 179
OC - Oceania 35
Continente sconosciuto - Info sul continente non disponibili 4
Totale 21.840
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 7.536
IT - Italia 3.594
RU - Federazione Russa 3.359
CN - Cina 1.206
SG - Singapore 1.189
BR - Brasile 638
VN - Vietnam 465
KR - Corea 359
FR - Francia 297
DE - Germania 256
JP - Giappone 228
SE - Svezia 194
NL - Olanda 188
GB - Regno Unito 178
FI - Finlandia 175
IE - Irlanda 156
CA - Canada 154
IN - India 130
AT - Austria 109
ES - Italia 109
BD - Bangladesh 79
HK - Hong Kong 76
PH - Filippine 71
TR - Turchia 67
UA - Ucraina 62
ID - Indonesia 60
CH - Svizzera 53
CI - Costa d'Avorio 50
MA - Marocco 47
AR - Argentina 45
JO - Giordania 38
MY - Malesia 38
TW - Taiwan 38
PL - Polonia 36
IQ - Iraq 34
BE - Belgio 30
MX - Messico 30
ZA - Sudafrica 30
TH - Thailandia 26
IR - Iran 25
SA - Arabia Saudita 24
AU - Australia 19
EC - Ecuador 19
PK - Pakistan 19
AE - Emirati Arabi Uniti 16
CL - Cile 16
NZ - Nuova Zelanda 16
EG - Egitto 12
CO - Colombia 11
UZ - Uzbekistan 11
GR - Grecia 10
KZ - Kazakistan 10
AZ - Azerbaigian 9
BJ - Benin 9
IL - Israele 9
VE - Venezuela 9
BO - Bolivia 8
DO - Repubblica Dominicana 8
KE - Kenya 8
CZ - Repubblica Ceca 6
LT - Lituania 6
NP - Nepal 6
PY - Paraguay 6
TT - Trinidad e Tobago 6
HU - Ungheria 5
PT - Portogallo 5
AL - Albania 4
DZ - Algeria 4
HN - Honduras 4
OM - Oman 4
PE - Perù 4
RO - Romania 4
TN - Tunisia 4
BG - Bulgaria 3
CR - Costa Rica 3
ET - Etiopia 3
MT - Malta 3
NO - Norvegia 3
PS - Palestinian Territory 3
QA - Qatar 3
RS - Serbia 3
SI - Slovenia 3
XK - ???statistics.table.value.countryCode.XK??? 3
BB - Barbados 2
BN - Brunei Darussalam 2
DK - Danimarca 2
GA - Gabon 2
JM - Giamaica 2
KG - Kirghizistan 2
KW - Kuwait 2
LB - Libano 2
LV - Lettonia 2
MK - Macedonia 2
MU - Mauritius 2
NG - Nigeria 2
SN - Senegal 2
SY - Repubblica araba siriana 2
AO - Angola 1
BA - Bosnia-Erzegovina 1
BH - Bahrain 1
Totale 21.827
Salva come PNG Salva come JPEG
Città #
Milan 1.427
Ashburn 1.051
San Jose 775
Singapore 709
Fairfield 483
Moscow 427
Chandler 376
Woodbridge 371
Santa Clara 327
Seoul 306
Hefei 279
Council Bluffs 242
Wilmington 241
Seattle 227
Beijing 216
Houston 213
The Dalles 209
Tokyo 194
Boardman 185
Cambridge 183
Ann Arbor 174
Dallas 174
Dublin 147
Los Angeles 111
Lauterbourg 104
Helsinki 102
Rome 96
Vienna 92
Ho Chi Minh City 91
Dearborn 87
Dong Ket 87
Ottawa 85
Amsterdam 84
Málaga 83
Lawrence 82
Medford 81
New York 80
Redwood City 78
Hanoi 68
Redmond 61
Buffalo 58
Davao City 58
Hong Kong 56
São Paulo 56
Frankfurt am Main 55
North Charleston 53
Abidjan 49
Ciampino 49
Bern 46
Monza 46
Jakarta 43
Gavirate 41
Orem 41
Jacksonville 40
Amman 38
Bovisio Masciago 38
Turin 38
Kent 34
Kuala Lumpur 34
Des Moines 31
Taipei 31
Las Vegas 29
Chennai 26
Nanjing 26
Segrate 26
Shanghai 26
Parma 25
Stockholm 25
Busto Arsizio 24
Chicago 24
Kenitra 24
London 24
Rio de Janeiro 24
Riverside 24
Istanbul 23
Marnate 23
Phoenix 23
Redondo Beach 23
Giussano 22
Pedrengo 22
San Diego 22
Brussels 21
Warsaw 21
Boltiere 20
Changsha 20
Islington 20
Trezzano Sul Naviglio 20
Arcene 19
Basingstoke 19
Bergamo 19
Washington 19
Brooklyn 18
Fremont 17
Lappeenranta 17
Montreal 15
San Francisco 15
Atlanta 14
Belo Horizonte 14
Berlin 14
Denver 14
Totale 12.164
Salva come PNG Salva come JPEG
Nome #
Accelerated ageing of micron- and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity 341
A Critical Analysis of Paraffin-based Fuel Formulations for Hybrid Rocket Propulsion 305
Aluminum powders: aging effects on metal content and thermogravimetry reactivity 304
Combustion Processes in Hybrid Rockets 299
Activated Aluminum Powders for Space Propulsion 298
A method for mechanical activation of powders by means of balls 293
Nickel acetylacetonate as decomposition catalyst for HTPB-based fuels: Regression rate enhancement effects 285
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 284
Iron oxide as solid propellant catalyst: A detailed characterization 284
Aerospace Propulsion Research Activities at SPlab. Overview and Results 283
Burning Behavior Investigation of a Vortex Flow Pancake Hybrid Rocket Engine 274
Paraffin-Based Fuels and Energetic Additives for Hybrid Rocket Propulsion 271
Green Fuels for Rocket Propulsion: Current Status and Future Perspectives of Paraffin-Based Formulations 270
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Ballistic characterization 265
Experimental data from ramjet/scramjet combustion and numerical validation perspectives 265
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part I, Mechanical and Pre-Burning Characterization 261
Experimental evaluation of HTPB/paraffin fuel blends for hybrid rocket applications 259
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Mechanical characterization 256
Evaluation of a Ramjet Model in a Supersonic High-Enthalpy Tunnel 245
Detailed Properties of Iron Oxide Solid Propellant Catalyst 237
Hybrid Combustion Studies on Regression Rate Enhancement and Transient Ballistic Response 237
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 236
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 236
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 233
A Comparative Study of the Aging Behavior of Different Nano-Sized Aluminum Powders 230
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 229
Role of Pressure and Aluminum Size in Solid Propellant CCP Generation 227
Influence of Operating Parameters on the Ballistics of a Lab-Scale Vortex Flow Pancake Hybrid Rocket Engine 227
Activated and Nano-Sized Aluminum as Metal Fuels in Solid Rocket Propellants 225
Hybrid Propulsion System for Future Rocket Applications 223
Cellular Structures for Solid Fuel Grain Reinforcement: Mechanical and Combustion Performance in Conventional and Non-Conventional Hybrid Rocket Engines 221
Trade-Off Analysis of a New Liquid Rocket Engine 220
Prospects of Aluminum Modifications as Energetic Fuels in Chemical Rocket Propulsion 217
Thermite-for-demise (T4D): experiments and numerical modelling on solar array drive mechanism mock-ups containing thermite in an arc-heated wind tunnel 213
Thermite-For-Demise (T4D): Material Selection for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 211
Analysis of Quasi-Steady and Transient Burning of Hybrid Fuels in a Laboratory-Scale Burner by an Optical Technique 210
Diagnostics for Entrainment Characterization in Liquefying Fuel Formulations 206
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 204
Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems 202
Towards High-Performing Paraffin-Based Fuels Exploiting the Armored Grain Concept 199
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part II, Ballistic Characterization 198
Aging Effects on Nano-Sized Aluminum Reactivity 197
Time-resolved burning of solid fuels for hybrid rocket propulsion 196
Thermite-for-demise (T4D): Experiments and numerical modelling on ball-bearing unit mock-ups containing thermite in an arc-heated wind tunnel 194
Liquid Film Cooling: Advanced Modeling and Efforts Towards Validation 191
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 191
Regression Rate and Combustion Efficiency in a Vortex-Flow Hybrid Rocket Engine 188
Micro and Nano-Sized Metal Additives for Solid Fuels in Hybrid Rocket Lab-Scale Burner 186
Combustion in a Lab-Scale Vortex Flow Hybrid Rocket Engine 186
Testing and Modeling Fuel Regression Rate in a Miniature Hybrid Burner 185
Non-Isothermal Oxidation of Aluminum Nanopowder Coated by Hydrocarbons and Fluorohydrocarbons 185
Lab-Scale Investigation of Metal Hydrides as Solid Fuel Additives for Hybrid Rocket Propulsion 184
Effect of Fluorides Coated Nano-Aluminum Powder on Combustion Properties of HTPB Based Fuels 184
Development of Paraffin-Based Fuels for a Vortex Combustion Hybrid Rocket Engine 181
Strategies for Paraffin-based Fuels Reinforcement: 3D Printing and Blending with Polymers 181
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 180
Numerical and experimental analysis of fuel regression rate in a lab-scale hybrid rocket engine with swirl injection 179
Impact of 3d-printing on the mechanical reinforcement and the ballistic response of paraffin-based fuels: The armored grain 178
Thermite-for-Demise (T4D): Preliminary Assessment on the Effects of a Thermite Charge in Arc-Heated Wind Tunnel Experiments 177
Liquefying Fuel Combustion in a Lab-scale Vortex Flow Pancake Hybrid Rocket Engine 177
Thermite-for-Demise: Preliminary on-Ground Heat Transfer Experimental Testing 176
Combustion in a Non-Conventional Hybrid Rocket Engine: Lab-Scale Testing of a Vortex Flow Pancake 174
Monte Carlo Analysis of a LEO Reentry Mission by Solid Rocket Propulsion 173
Combustion of HTPB-Based Solid Fuels Loaded with Coated Nanoaluminum 168
Liquid Film Cooling: Open-Literature Review, Modeling and Efforts Towards Validation 167
Time-resolved regression rate of innovative hybrid solid fuel formulations 166
Novel Activated Metal Powders for Improved Hybrid Fuels and Green Solid Propellants 166
Thermite-for-Demise (T4D): from Material Selection to Test Campaign 165
Ballistic Characterization of Armored Grains with Vortex Flow Pancake Hybrid Rocket Engine 165
Vortex combustion in a hybrid rocket motor 163
Thermite-for-Demise (T4D): Concept Definition for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 163
Hydrogen-Based Thrusters for Supersonic and Hypersonic Flight: Experimental Characterization 162
Reduction of Solid Propellants Environmental Impact: Al-Mg Mechanically Activated Fuels and AP-PSAN Blends 159
Experimental Investigation of a H2O2 Hybrid Rocket with Different Swirl Injections and Fuels 158
Preparation and Characterization of Al/HTPB Composite for High Energetic Materials 158
Mechanically Activated Al/Mg Powders for Solid Rocket Propellants 155
Aggregation and Incipient Agglomeration in Metallized Solid Propellants and Solid Fuels for Rocket Propulsion 152
Boosting Green Propellants: the Sustainable Armored Grain for Hybrid Rocket Propulsion 151
METODO PER LA LAVORAZIONE E/O L'ATTIVAZIONE MECCANICA DI POLVERI TRAMITE SFERE 151
Effects of Vortex Flow Pancake Hybrid Rocket Engine Operating Parameters on Liquefying Fuel Combustion 149
Development of a Compact Hybrid Rocket Engine for Low-Cost In-Space Propulsion 149
Test Activities on Hybrid Rocket Engines: Combustion Analyses and Green Storable Oxidizers - A Short Review 149
Comparison Between Nano-Sized Aluminum Powders with Different Coatings: Physical Analyses and Performance Test 148
Regression Rate and CCPs Measurement of Metallized Solid Fuels 146
Nano-Sized and Mechanically Activated Composites: Perspectives for Enhanced Mass Burning Rate in Aluminized Solid Fuels for Hybrid Rocket Propulsion 145
Reconstructed Ballistic Data Versus Wax Regression-Rate Intrusive Measurement in a Hybrid Rocket 144
Mapping of Aluminum Particle Dispersion in Solid Rocket Fuel Formulations 138
Regression Rate Measurements in Lab-Scale Hybrid Burners 137
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 136
Paraffin-Based Fuels: Perspectives from Different Reinforcing Strategies and Metal Additives 134
Experimental activities on the paraffin-based fuel MTM in the framework of the PHAEDRA project 134
Numerical and Experimental Investigation of a Lab-Scale Paraffin Motor with Swirled Injection of Gaseous Oxygen 133
Green Solid Fuels with Enhanced Mechanical Properties: Sustainable Waxes and Scale-Up Analysis of Armored Grains 131
Hydrolytic Space Propulsion: a New Opportunity for CubeSat Missions 128
Mixed-Hybrid Fuel Formulations: Composition, Regression Rate and Condensed Combustion Products 127
Innovative Methodology for Evaluating Combustion Efficiency in Swirled Rocket Engines 125
Testing Advanced Green Thermoplastic Fuels in a Vortex Hybrid Rocket Engine 125
Diagnostic Techniques for Regression Rate of Paraffin-Based Fuels in a VFP Hybrid Rocket Engine 123
Effects of Grain Cracks on the Combustion of a VFP Engine Burning Paraffin-based Fuels 121
Ignition and combustion of hydroxyl-terminated polybutadiene (HTPB)-based solid fuels loaded with innovative micrometer-sized metals 121
Totale 19.638
Salva come PNG Salva come JPEG
Categoria #
all - tutte 54.966
article - articoli 13.998
book - libri 0
conference - conferenze 36.096
curatela - curatele 0
other - altro 0
patent - brevetti 1.022
selected - selezionate 0
volume - volumi 3.850
Totale 109.932
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021215 0 0 0 0 0 0 0 0 0 0 0 215
2021/2022974 57 104 93 48 90 64 70 100 32 71 119 126
2022/20231.417 155 112 64 122 143 130 47 109 212 150 67 106
2023/2024876 72 119 37 98 56 110 111 43 36 66 53 75
2024/20253.830 150 58 141 131 710 164 187 316 336 170 450 1.017
2025/20269.857 2.044 1.423 590 603 397 576 1.370 647 666 886 358 297
Totale 22.013