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

PARAVAN, CHRISTIAN
 Distribuzione geografica
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Continente #
EU - Europa 9.359
NA - Nord America 8.409
AS - Asia 4.331
SA - Sud America 776
AF - Africa 179
Continente sconosciuto - Info sul continente non disponibili 178
OC - Oceania 35
Totale 23.267
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Nazione #
US - Stati Uniti d'America 8.138
IT - Italia 4.074
RU - Federazione Russa 3.360
CN - Cina 1.224
SG - Singapore 1.195
BR - Brasile 651
VN - Vietnam 493
KR - Corea 360
FR - Francia 299
DE - Germania 257
JP - Giappone 229
SE - Svezia 195
NL - Olanda 190
GB - Regno Unito 180
FI - Finlandia 175
CA - Canada 174
IE - Irlanda 156
IN - India 136
ES - Italia 111
AT - Austria 109
BD - Bangladesh 81
HK - Hong Kong 77
PH - Filippine 71
TR - Turchia 67
UA - Ucraina 62
ID - Indonesia 60
CH - Svizzera 53
CI - Costa d'Avorio 50
AR - Argentina 48
MA - Marocco 47
TW - Taiwan 42
JO - Giordania 38
MY - Malesia 38
PL - Polonia 38
MX - Messico 35
IQ - Iraq 34
BE - Belgio 31
ZA - Sudafrica 30
TH - Thailandia 29
IR - Iran 25
SA - Arabia Saudita 24
AU - Australia 19
EC - Ecuador 19
PK - Pakistan 19
CL - Cile 17
AE - Emirati Arabi Uniti 16
NZ - Nuova Zelanda 16
EG - Egitto 12
IL - Israele 12
CO - Colombia 11
JM - Giamaica 11
UZ - Uzbekistan 11
GR - Grecia 10
KZ - Kazakistan 10
AZ - Azerbaigian 9
BJ - Benin 9
TT - Trinidad e Tobago 9
VE - Venezuela 9
BO - Bolivia 8
DO - Repubblica Dominicana 8
KE - Kenya 8
PY - Paraguay 8
CR - Costa Rica 7
HN - Honduras 7
PT - Portogallo 7
CZ - Repubblica Ceca 6
LT - Lituania 6
NP - Nepal 6
HU - Ungheria 5
AL - Albania 4
DZ - Algeria 4
NI - Nicaragua 4
OM - Oman 4
PE - Perù 4
RO - Romania 4
TN - Tunisia 4
BB - Barbados 3
BG - Bulgaria 3
BN - Brunei Darussalam 3
BZ - Belize 3
ET - Etiopia 3
MT - Malta 3
NO - Norvegia 3
PS - Palestinian Territory 3
QA - Qatar 3
RS - Serbia 3
SI - Slovenia 3
SV - El Salvador 3
XK - ???statistics.table.value.countryCode.XK??? 3
BA - Bosnia-Erzegovina 2
DK - Danimarca 2
GA - Gabon 2
KG - Kirghizistan 2
KW - Kuwait 2
LB - Libano 2
LV - Lettonia 2
MK - Macedonia 2
MU - Mauritius 2
NG - Nigeria 2
PR - Porto Rico 2
Totale 23.070
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Città #
Milan 1.632
Ashburn 1.120
San Jose 792
Singapore 712
Fairfield 483
Moscow 427
Chandler 376
Woodbridge 371
Council Bluffs 339
Santa Clara 339
Seoul 306
Hefei 279
Wilmington 241
Seattle 228
Beijing 222
Houston 216
The Dalles 209
Tokyo 194
Boardman 185
Cambridge 183
Dallas 183
Ann Arbor 174
Rome 151
Dublin 147
Los Angeles 121
Lauterbourg 104
Helsinki 102
Ho Chi Minh City 99
Vienna 92
Dearborn 88
New York 88
Dong Ket 87
Medford 85
Ottawa 85
Amsterdam 84
Málaga 83
Lawrence 82
Redwood City 78
Hanoi 76
Redmond 61
Buffalo 59
São Paulo 59
Davao City 58
Hong Kong 56
Frankfurt am Main 55
North Charleston 53
Abidjan 49
Ciampino 49
Turin 48
Bern 46
Monza 46
Jakarta 43
Jacksonville 42
Gavirate 41
Orem 41
Amman 38
Bovisio Masciago 38
Chicago 37
Kent 34
Kuala Lumpur 34
Las Vegas 33
Des Moines 31
Phoenix 31
Taipei 31
Shanghai 27
Chennai 26
Nanjing 26
Parma 26
Rio de Janeiro 26
Segrate 26
Stockholm 26
London 25
Naples 25
Riverside 25
Busto Arsizio 24
Kenitra 24
Istanbul 23
Marnate 23
Redondo Beach 23
San Diego 23
Warsaw 23
Washington 23
Brooklyn 22
Giussano 22
Pedrengo 22
Brussels 21
Bergamo 20
Boltiere 20
Changsha 20
Islington 20
Montreal 20
Trezzano Sul Naviglio 20
Arcene 19
Basingstoke 19
Bologna 19
Xi'an 18
Atlanta 17
Denver 17
Fremont 17
Lappeenranta 17
Totale 12.770
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Nome #
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 315
Nickel acetylacetonate as decomposition catalyst for HTPB-based fuels: Regression rate enhancement effects 310
Activated Aluminum Powders for Space Propulsion 306
Combustion Processes in Hybrid Rockets 306
A method for mechanical activation of powders by means of balls 302
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
Burning Behavior Investigation of a Vortex Flow Pancake Hybrid Rocket Engine 278
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Ballistic characterization 273
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 268
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part I, Mechanical and Pre-Burning Characterization 265
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Mechanical characterization 264
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
A Comparative Study of the Aging Behavior of Different Nano-Sized Aluminum Powders 242
Hybrid Combustion Studies on Regression Rate Enhancement and Transient Ballistic Response 242
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
Hybrid Propulsion System for Future Rocket Applications 231
Thermite-for-demise (T4D): experiments and numerical modelling on solar array drive mechanism mock-ups containing thermite in an arc-heated wind tunnel 231
Role of Pressure and Aluminum Size in Solid Propellant CCP Generation 231
Prospects of Aluminum Modifications as Energetic Fuels in Chemical Rocket Propulsion 230
Cellular Structures for Solid Fuel Grain Reinforcement: Mechanical and Combustion Performance in Conventional and Non-Conventional Hybrid Rocket Engines 228
Trade-Off Analysis of a New Liquid Rocket Engine 227
Analysis of Quasi-Steady and Transient Burning of Hybrid Fuels in a Laboratory-Scale Burner by an Optical Technique 223
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part II, Ballistic Characterization 219
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
Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems 205
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 205
Lab-Scale Investigation of Metal Hydrides as Solid Fuel Additives for Hybrid Rocket Propulsion 204
Thermite-for-demise (T4D): Experiments and numerical modelling on ball-bearing unit mock-ups containing thermite in an arc-heated wind tunnel 202
Aging Effects on Nano-Sized Aluminum Reactivity 202
Time-resolved burning of solid fuels for hybrid rocket propulsion 200
Combustion in a Lab-Scale Vortex Flow Hybrid Rocket Engine 198
Liquid Film Cooling: Advanced Modeling and Efforts Towards Validation 195
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 195
Testing and Modeling Fuel Regression Rate in a Miniature Hybrid Burner 192
Development of Paraffin-Based Fuels for a Vortex Combustion Hybrid Rocket Engine 191
Micro and Nano-Sized Metal Additives for Solid Fuels in Hybrid Rocket Lab-Scale Burner 190
Non-Isothermal Oxidation of Aluminum Nanopowder Coated by Hydrocarbons and Fluorohydrocarbons 190
Strategies for Paraffin-based Fuels Reinforcement: 3D Printing and Blending with Polymers 190
Combustion in a Non-Conventional Hybrid Rocket Engine: Lab-Scale Testing of a Vortex Flow Pancake 188
Effect of Fluorides Coated Nano-Aluminum Powder on Combustion Properties of HTPB Based Fuels 187
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 187
Numerical and experimental analysis of fuel regression rate in a lab-scale hybrid rocket engine with swirl injection 185
Liquid Film Cooling: Open-Literature Review, Modeling and Efforts Towards Validation 184
Impact of 3d-printing on the mechanical reinforcement and the ballistic response of paraffin-based fuels: The armored grain 184
Thermite-for-Demise: Preliminary on-Ground Heat Transfer Experimental Testing 183
Liquefying Fuel Combustion in a Lab-scale Vortex Flow Pancake Hybrid Rocket Engine 183
Ballistic Characterization of Armored Grains with Vortex Flow Pancake Hybrid Rocket Engine 181
Thermite-for-Demise (T4D): Preliminary Assessment on the Effects of a Thermite Charge in Arc-Heated Wind Tunnel Experiments 179
Novel Activated Metal Powders for Improved Hybrid Fuels and Green Solid Propellants 178
Monte Carlo Analysis of a LEO Reentry Mission by Solid Rocket Propulsion 177
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
Thermite-for-Demise (T4D): from Material Selection to Test Campaign 171
Combustion of HTPB-Based Solid Fuels Loaded with Coated Nanoaluminum 171
Hydrogen-Based Thrusters for Supersonic and Hypersonic Flight: Experimental Characterization 171
Time-resolved regression rate of innovative hybrid solid fuel formulations 169
Experimental Investigation of a H2O2 Hybrid Rocket with Different Swirl Injections and Fuels 166
Boosting Green Propellants: the Sustainable Armored Grain for Hybrid Rocket Propulsion 165
Effects of Vortex Flow Pancake Hybrid Rocket Engine Operating Parameters on Liquefying Fuel Combustion 162
Mechanically Activated Al/Mg Powders for Solid Rocket Propellants 162
Test Activities on Hybrid Rocket Engines: Combustion Analyses and Green Storable Oxidizers - A Short Review 161
Preparation and Characterization of Al/HTPB Composite for High Energetic Materials 159
Aggregation and Incipient Agglomeration in Metallized Solid Propellants and Solid Fuels for Rocket Propulsion 158
Comparison Between Nano-Sized Aluminum Powders with Different Coatings: Physical Analyses and Performance Test 155
Regression Rate and CCPs Measurement of Metallized Solid Fuels 154
Reconstructed Ballistic Data Versus Wax Regression-Rate Intrusive Measurement in a Hybrid Rocket 153
Experimental activities on the paraffin-based fuel MTM in the framework of the PHAEDRA project 152
Development of a Compact Hybrid Rocket Engine for Low-Cost In-Space Propulsion 152
METODO PER LA LAVORAZIONE E/O L'ATTIVAZIONE MECCANICA DI POLVERI TRAMITE SFERE 151
Nano-Sized and Mechanically Activated Composites: Perspectives for Enhanced Mass Burning Rate in Aluminized Solid Fuels for Hybrid Rocket Propulsion 146
Hydrolytic Space Propulsion: a New Opportunity for CubeSat Missions 145
Numerical and Experimental Investigation of a Lab-Scale Paraffin Motor with Swirled Injection of Gaseous Oxygen 143
Regression Rate Measurements in Lab-Scale Hybrid Burners 142
Paraffin-Based Fuels: Perspectives from Different Reinforcing Strategies and Metal Additives 141
Testing Advanced Green Thermoplastic Fuels in a Vortex Hybrid Rocket Engine 141
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 140
Mapping of Aluminum Particle Dispersion in Solid Rocket Fuel Formulations 140
Innovative Methodology for Evaluating Combustion Efficiency in Swirled Rocket Engines 139
Green Solid Fuels with Enhanced Mechanical Properties: Sustainable Waxes and Scale-Up Analysis of Armored Grains 138
Coated Nano-Sized Aluminum Powders: Physical Analyses and Performance Tests in Hybrid Propulsion 133
Quasi-steady and Forced Transient Burning of a Vortex Flow Hybrid Motor 130
Mixed-Hybrid Fuel Formulations: Composition, Regression Rate and Condensed Combustion Products 130
Ignition and combustion of hydroxyl-terminated polybutadiene (HTPB)-based solid fuels loaded with innovative micrometer-sized metals 130
Totale 20.500
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Categoria #
all - tutte 58.308
article - articoli 14.680
book - libri 0
conference - conferenze 38.539
curatela - curatele 0
other - altro 0
patent - brevetti 1.058
selected - selezionate 0
volume - volumi 4.031
Totale 116.616
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022917 0 104 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
2025/202610.333 2.044 1.423 590 603 397 576 1.370 647 666 886 358 773
2026/2027778 467 311 0 0 0 0 0 0 0 0 0 0
Totale 23.267