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

PARAVAN, CHRISTIAN
 Distribuzione geografica
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Continente #
EU - Europa 7.903
NA - Nord America 5.595
AS - Asia 2.756
SA - Sud America 693
AF - Africa 134
OC - Oceania 31
Continente sconosciuto - Info sul continente non disponibili 2
Totale 17.114
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Nazione #
US - Stati Uniti d'America 5.434
RU - Federazione Russa 3.357
IT - Italia 3.063
CN - Cina 892
SG - Singapore 851
BR - Brasile 602
VN - Vietnam 268
DE - Germania 223
SE - Svezia 178
FR - Francia 170
FI - Finlandia 142
NL - Olanda 138
KR - Corea 137
IE - Irlanda 126
CA - Canada 123
GB - Regno Unito 114
IN - India 109
ES - Italia 100
AT - Austria 85
PH - Filippine 66
UA - Ucraina 61
TR - Turchia 53
CH - Svizzera 51
ID - Indonesia 51
CI - Costa d'Avorio 49
HK - Hong Kong 44
BD - Bangladesh 43
AR - Argentina 42
JP - Giappone 41
JO - Giordania 36
BE - Belgio 29
ZA - Sudafrica 24
IR - Iran 22
PL - Polonia 22
SA - Arabia Saudita 20
MA - Marocco 19
MX - Messico 19
TW - Taiwan 18
IQ - Iraq 17
AU - Australia 16
EC - Ecuador 16
NZ - Nuova Zelanda 15
AE - Emirati Arabi Uniti 14
PK - Pakistan 14
EG - Egitto 11
CO - Colombia 10
UZ - Uzbekistan 10
BJ - Benin 9
KZ - Kazakistan 9
AZ - Azerbaigian 8
GR - Grecia 8
IL - Israele 8
DO - Repubblica Dominicana 7
MY - Malesia 6
VE - Venezuela 6
CL - Cile 5
HU - Ungheria 5
PY - Paraguay 5
AL - Albania 4
BO - Bolivia 4
CZ - Repubblica Ceca 4
DZ - Algeria 4
HN - Honduras 4
KE - Kenya 4
LT - Lituania 4
OM - Oman 4
TN - Tunisia 4
NO - Norvegia 3
PT - Portogallo 3
TH - Thailandia 3
TT - Trinidad e Tobago 3
CR - Costa Rica 2
DK - Danimarca 2
ET - Etiopia 2
JM - Giamaica 2
KG - Kirghizistan 2
LB - Libano 2
MT - Malta 2
MU - Mauritius 2
NG - Nigeria 2
PE - Perù 2
PS - Palestinian Territory 2
QA - Qatar 2
RO - Romania 2
RS - Serbia 2
SN - Senegal 2
BA - Bosnia-Erzegovina 1
BG - Bulgaria 1
BN - Brunei Darussalam 1
BW - Botswana 1
EE - Estonia 1
EU - Europa 1
KW - Kuwait 1
LA - Repubblica Popolare Democratica del Laos 1
LV - Lettonia 1
NP - Nepal 1
PA - Panama 1
SD - Sudan 1
SK - Slovacchia (Repubblica Slovacca) 1
SR - Suriname 1
Totale 17.113
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Città #
Milan 1.105
Ashburn 744
Singapore 506
Fairfield 483
Moscow 426
Chandler 376
Woodbridge 370
Santa Clara 291
Hefei 278
Wilmington 241
Seattle 225
Houston 208
Cambridge 183
Beijing 182
Ann Arbor 174
Council Bluffs 130
Boardman 118
Dublin 117
Rome 93
Dearborn 87
Dong Ket 87
Seoul 87
Ottawa 85
Málaga 83
Lawrence 82
Medford 81
Los Angeles 78
Redwood City 78
Helsinki 69
Vienna 68
New York 62
Redmond 61
Dallas 59
Davao City 58
Amsterdam 54
Buffalo 52
São Paulo 50
Ciampino 49
Abidjan 48
Bern 46
Monza 46
Gavirate 41
Jakarta 41
Jacksonville 40
Bovisio Masciago 38
Ho Chi Minh City 37
Amman 36
Frankfurt am Main 34
Kent 34
Des Moines 30
The Dalles 27
Hong Kong 26
Segrate 26
Nanjing 25
Riverside 24
Hanoi 23
Marnate 23
Parma 23
Redondo Beach 23
Giussano 22
Pedrengo 22
Chennai 21
San Diego 21
Turin 21
Boltiere 20
Brussels 20
Istanbul 20
Rio de Janeiro 20
Trezzano Sul Naviglio 20
Arcene 19
Bergamo 19
Lappeenranta 17
Fremont 16
London 16
Tokyo 16
Berlin 14
Mumbai 14
Norwalk 14
Washington 14
Belo Horizonte 13
Brooklyn 13
Hyderabad 13
Nave 13
Phoenix 13
Shanghai 13
Taipei 13
Torre Del Greco 13
Tradate 13
Aţ Ţuwāl 12
College Station 12
Dhaka 12
Stockholm 12
West Lafayette 12
Changsha 11
Chicago 11
Novara 11
Auckland 10
Baveno 10
Brasília 10
Bresso 10
Totale 8.887
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Nome #
Accelerated ageing of micron- and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity 278
Combustion Processes in Hybrid Rockets 261
Activated Aluminum Powders for Space Propulsion 258
Iron oxide as solid propellant catalyst: A detailed characterization 252
Aerospace Propulsion Research Activities at SPlab. Overview and Results 246
A method for mechanical activation of powders by means of balls 245
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 244
Aluminum powders: aging effects on metal content and thermogravimetry reactivity 244
A Critical Analysis of Paraffin-based Fuel Formulations for Hybrid Rocket Propulsion 243
Burning Behavior Investigation of a Vortex Flow Pancake Hybrid Rocket Engine 242
Green Fuels for Rocket Propulsion: Current Status and Future Perspectives of Paraffin-Based Formulations 241
Experimental data from ramjet/scramjet combustion and numerical validation perspectives 229
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part I, Mechanical and Pre-Burning Characterization 223
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Mechanical characterization 208
Paraffin-Based Fuels and Energetic Additives for Hybrid Rocket Propulsion 206
Hybrid Combustion Studies on Regression Rate Enhancement and Transient Ballistic Response 201
Evaluation of a Ramjet Model in a Supersonic High-Enthalpy Tunnel 201
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 199
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 199
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 199
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Ballistic characterization 197
Role of Pressure and Aluminum Size in Solid Propellant CCP Generation 196
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 196
Trade-Off Analysis of a New Liquid Rocket Engine 194
Experimental evaluation of HTPB/paraffin fuel blends for hybrid rocket applications 194
Detailed Properties of Iron Oxide Solid Propellant Catalyst 193
Analysis of Quasi-Steady and Transient Burning of Hybrid Fuels in a Laboratory-Scale Burner by an Optical Technique 189
Hybrid Propulsion System for Future Rocket Applications 187
A Comparative Study of the Aging Behavior of Different Nano-Sized Aluminum Powders 187
Cellular Structures for Solid Fuel Grain Reinforcement: Mechanical and Combustion Performance in Conventional and Non-Conventional Hybrid Rocket Engines 186
Prospects of Aluminum Modifications as Energetic Fuels in Chemical Rocket Propulsion 184
Influence of Operating Parameters on the Ballistics of a Lab-Scale Vortex Flow Pancake Hybrid Rocket Engine 181
Thermite-For-Demise (T4D): Material Selection for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 177
Diagnostics for Entrainment Characterization in Liquefying Fuel Formulations 172
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 170
Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems 169
Time-resolved burning of solid fuels for hybrid rocket propulsion 168
Towards High-Performing Paraffin-Based Fuels Exploiting the Armored Grain Concept 167
Regression Rate and Combustion Efficiency in a Vortex-Flow Hybrid Rocket Engine 165
Micro and Nano-Sized Metal Additives for Solid Fuels in Hybrid Rocket Lab-Scale Burner 164
Activated and Nano-Sized Aluminum as Metal Fuels in Solid Rocket Propellants 164
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 163
Testing and Modeling Fuel Regression Rate in a Miniature Hybrid Burner 160
Combustion in a Lab-Scale Vortex Flow Hybrid Rocket Engine 159
Non-Isothermal Oxidation of Aluminum Nanopowder Coated by Hydrocarbons and Fluorohydrocarbons 158
Aging Effects on Nano-Sized Aluminum Reactivity 158
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part II, Ballistic Characterization 156
Lab-Scale Investigation of Metal Hydrides as Solid Fuel Additives for Hybrid Rocket Propulsion 155
Effect of Fluorides Coated Nano-Aluminum Powder on Combustion Properties of HTPB Based Fuels 155
Strategies for Paraffin-based Fuels Reinforcement: 3D Printing and Blending with Polymers 155
Thermite-for-demise (T4D): Experiments and numerical modelling on ball-bearing unit mock-ups containing thermite in an arc-heated wind tunnel 154
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 154
Liquid Film Cooling: Advanced Modeling and Efforts Towards Validation 150
Liquefying Fuel Combustion in a Lab-scale Vortex Flow Pancake Hybrid Rocket Engine 149
Monte Carlo Analysis of a LEO Reentry Mission by Solid Rocket Propulsion 148
Impact of 3d-printing on the mechanical reinforcement and the ballistic response of paraffin-based fuels: The armored grain 146
Novel Activated Metal Powders for Improved Hybrid Fuels and Green Solid Propellants 144
Thermite-for-Demise: Preliminary on-Ground Heat Transfer Experimental Testing 143
Combustion of HTPB-Based Solid Fuels Loaded with Coated Nanoaluminum 142
Numerical and experimental analysis of fuel regression rate in a lab-scale hybrid rocket engine with swirl injection 139
Development of Paraffin-Based Fuels for a Vortex Combustion Hybrid Rocket Engine 136
Combustion in a Non-Conventional Hybrid Rocket Engine: Lab-Scale Testing of a Vortex Flow Pancake 134
Hydrogen-Based Thrusters for Supersonic and Hypersonic Flight: Experimental Characterization 134
Time-resolved regression rate of innovative hybrid solid fuel formulations 133
Vortex combustion in a hybrid rocket motor 133
Thermite-for-Demise (T4D): from Material Selection to Test Campaign 131
Thermite-for-Demise (T4D): Preliminary Assessment on the Effects of a Thermite Charge in Arc-Heated Wind Tunnel Experiments 131
Ballistic Characterization of Armored Grains with Vortex Flow Pancake Hybrid Rocket Engine 131
Thermite-for-Demise (T4D): Concept Definition for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 131
Comparison Between Nano-Sized Aluminum Powders with Different Coatings: Physical Analyses and Performance Test 129
Reduction of Solid Propellants Environmental Impact: Al-Mg Mechanically Activated Fuels and AP-PSAN Blends 129
Liquid Film Cooling: Open-Literature Review, Modeling and Efforts Towards Validation 128
Experimental Investigation of a H2O2 Hybrid Rocket with Different Swirl Injections and Fuels 127
Nano-Sized and Mechanically Activated Composites: Perspectives for Enhanced Mass Burning Rate in Aluminized Solid Fuels for Hybrid Rocket Propulsion 126
Aggregation and Incipient Agglomeration in Metallized Solid Propellants and Solid Fuels for Rocket Propulsion 125
METODO PER LA LAVORAZIONE E/O L'ATTIVAZIONE MECCANICA DI POLVERI TRAMITE SFERE 125
Boosting Green Propellants: the Sustainable Armored Grain for Hybrid Rocket Propulsion 122
Preparation and Characterization of Al/HTPB Composite for High Energetic Materials 122
Thermite-for-demise (T4D): experiments and numerical modelling on solar array drive mechanism mock-ups containing thermite in an arc-heated wind tunnel 119
Mechanically Activated Al/Mg Powders for Solid Rocket Propellants 119
Nickel acetylacetonate as decomposition catalyst for HTPB-based fuels: Regression rate enhancement effects 118
Regression Rate and CCPs Measurement of Metallized Solid Fuels 117
Development of a Compact Hybrid Rocket Engine for Low-Cost In-Space Propulsion 117
Reconstructed Ballistic Data Versus Wax Regression-Rate Intrusive Measurement in a Hybrid Rocket 117
Test Activities on Hybrid Rocket Engines: Combustion Analyses and Green Storable Oxidizers - A Short Review 117
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 116
Effects of Vortex Flow Pancake Hybrid Rocket Engine Operating Parameters on Liquefying Fuel Combustion 115
Experimental activities on the paraffin-based fuel MTM in the framework of the PHAEDRA project 113
Regression Rate Measurements in Lab-Scale Hybrid Burners 113
Paraffin-Based Fuels: Perspectives from Different Reinforcing Strategies and Metal Additives 110
Numerical and Experimental Investigation of a Lab-Scale Paraffin Motor with Swirled Injection of Gaseous Oxygen 106
Mapping of Aluminum Particle Dispersion in Solid Rocket Fuel Formulations 105
Diagnostic Techniques for Regression Rate of Paraffin-Based Fuels in a VFP Hybrid Rocket Engine 104
Mixed-Hybrid Fuel Formulations: Composition, Regression Rate and Condensed Combustion Products 102
Hydrolytic Space Propulsion: a New Opportunity for CubeSat Missions 100
Anisotropy Effects in Hybrid Fuels Burning in a Microburner 100
Quasi-steady and Forced Transient Burning of a Vortex Flow Hybrid Motor 98
Testing Advanced Green Thermoplastic Fuels in a Vortex Hybrid Rocket Engine 98
Nanometric Powders Dispersion in a Polymeric Matrix 97
Coated Nano-Sized Aluminum Powders: Physical Analyses and Performance Tests in Hybrid Propulsion 97
Totale 16.032
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Categoria #
all - tutte 45.209
article - articoli 11.752
book - libri 0
conference - conferenze 29.294
curatela - curatele 0
other - altro 0
patent - brevetti 862
selected - selezionate 0
volume - volumi 3.301
Totale 90.418
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021863 0 0 0 0 0 196 89 94 76 97 96 215
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
2025/20265.112 2.044 1.423 590 603 397 55 0 0 0 0 0 0
Totale 17.268