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

PARAVAN, CHRISTIAN
 Distribuzione geografica
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Continente #
NA - Nord America 3.955
EU - Europa 3.553
AS - Asia 801
AF - Africa 49
SA - Sud America 19
OC - Oceania 15
Continente sconosciuto - Info sul continente non disponibili 1
Totale 8.393
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Nazione #
US - Stati Uniti d'America 3.855
IT - Italia 2.496
SE - Svezia 166
VN - Vietnam 158
CN - Cina 148
DE - Germania 133
FI - Finlandia 118
SG - Singapore 113
CA - Canada 98
IE - Irlanda 97
ES - Italia 87
IN - India 84
GB - Regno Unito 83
FR - Francia 77
KR - Corea 75
PH - Filippine 58
UA - Ucraina 57
RU - Federazione Russa 56
CH - Svizzera 51
AT - Austria 50
CI - Costa d'Avorio 38
JO - Giordania 36
NL - Olanda 34
TR - Turchia 27
BE - Belgio 22
HK - Hong Kong 19
IR - Iran 19
JP - Giappone 19
BR - Brasile 15
TW - Taiwan 13
NZ - Nuova Zelanda 10
AE - Emirati Arabi Uniti 9
PL - Polonia 8
GR - Grecia 7
MY - Malesia 6
AU - Australia 5
ID - Indonesia 5
EG - Egitto 4
IL - Israele 4
HU - Ungheria 3
PK - Pakistan 3
AR - Argentina 2
BD - Bangladesh 2
BO - Bolivia 2
CZ - Repubblica Ceca 2
MT - Malta 2
MU - Mauritius 2
MX - Messico 2
NG - Nigeria 2
NO - Norvegia 2
TH - Thailandia 2
BA - Bosnia-Erzegovina 1
EU - Europa 1
KE - Kenya 1
MA - Marocco 1
OM - Oman 1
RO - Romania 1
SD - Sudan 1
Totale 8.393
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Città #
Milan 761
Fairfield 483
Chandler 376
Woodbridge 370
Ashburn 302
Wilmington 240
Seattle 221
Houston 205
Cambridge 183
Ann Arbor 174
Dublin 89
Dearborn 87
Dong Ket 87
Ottawa 84
Málaga 83
Lawrence 82
Rome 82
Medford 81
Redwood City 78
Helsinki 64
Singapore 64
Redmond 61
Davao City 58
Ciampino 49
Bern 46
Beijing 44
Gavirate 41
Vienna 40
Abidjan 38
Bovisio Masciago 38
Jacksonville 38
Amman 36
Monza 36
New York 36
Des Moines 30
Seoul 28
Segrate 26
Nanjing 24
Riverside 24
Marnate 23
Giussano 22
San Diego 21
Trezzano Sul Naviglio 20
Amsterdam 19
Arcene 19
Bergamo 19
Turin 18
Chennai 17
Brussels 16
Fremont 16
Berlin 14
Norwalk 14
Nave 13
Taipei 13
Torre Del Greco 13
Tradate 13
Washington 13
Moscow 12
Mumbai 12
Parma 12
College Station 11
London 11
Novara 11
Baveno 10
Bresso 10
Mountain View 10
Varese 10
Venegono Superiore 10
Frankfurt am Main 9
Reggio Emilia 9
West Lafayette 9
Besana in Brianza 8
Boardman 8
Duncan 8
Genzano Di Roma 8
Hyderabad 8
San Giuliano Milanese 8
Seregno 8
Shanghai 8
Toulouse 8
Auckland 7
Istanbul 7
Kunming 7
Lappeenranta 7
Naples 7
Olgiate Comasco 7
Oulu 7
Ankara 6
Auburn Hills 6
Central 6
Kharagpur 6
Magenta 6
Rho 6
Velletri 6
Wayne 6
Zanica 6
Aberdeen 5
Al Ain City 5
Avezzano 5
Cormano 5
Totale 5.533
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Nome #
Iron oxide as solid propellant catalyst: A detailed characterization 213
Burning Behavior Investigation of a Vortex Flow Pancake Hybrid Rocket Engine 186
Accelerated ageing of micron- and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity 183
Activated Aluminum Powders for Space Propulsion 179
Combustion Processes in Hybrid Rockets 178
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 160
A Critical Analysis of Paraffin-based Fuel Formulations for Hybrid Rocket Propulsion 157
A method for mechanical activation of powders by means of balls 153
Experimental data from ramjet/scramjet combustion and numerical validation perspectives 152
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part I, Mechanical and Pre-Burning Characterization 150
Aluminum powders: aging effects on metal content and thermogravimetry reactivity 148
Role of Pressure and Aluminum Size in Solid Propellant CCP Generation 147
Paraffin-Based Fuels and Energetic Additives for Hybrid Rocket Propulsion 146
Aerospace Propulsion Research Activities at SPlab. Overview and Results 146
Green Fuels for Rocket Propulsion: Current Status and Future Perspectives of Paraffin-Based Formulations 139
Prospects of Aluminum Modifications as Energetic Fuels in Chemical Rocket Propulsion 137
Hybrid Combustion Studies on Regression Rate Enhancement and Transient Ballistic Response 137
Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems 133
Trade-Off Analysis of a New Liquid Rocket Engine 132
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 131
Testing and Modeling Fuel Regression Rate in a Miniature Hybrid Burner 126
Analysis of Quasi-Steady and Transient Burning of Hybrid Fuels in a Laboratory-Scale Burner by an Optical Technique 126
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 126
Detailed Properties of Iron Oxide Solid Propellant Catalyst 124
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 124
Non-Isothermal Oxidation of Aluminum Nanopowder Coated by Hydrocarbons and Fluorohydrocarbons 123
Influence of Operating Parameters on the Ballistics of a Lab-Scale Vortex Flow Pancake Hybrid Rocket Engine 118
Micro and Nano-Sized Metal Additives for Solid Fuels in Hybrid Rocket Lab-Scale Burner 111
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 109
Time-resolved burning of solid fuels for hybrid rocket propulsion 108
Combustion of HTPB-Based Solid Fuels Loaded with Coated Nanoaluminum 108
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 107
Evaluation of a Ramjet Model in a Supersonic High-Enthalpy Tunnel 104
Effect of Fluorides Coated Nano-Aluminum Powder on Combustion Properties of HTPB Based Fuels 103
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 101
Diagnostics for Entrainment Characterization in Liquefying Fuel Formulations 101
Combustion in a Lab-Scale Vortex Flow Hybrid Rocket Engine 98
Regression Rate and Combustion Efficiency in a Vortex-Flow Hybrid Rocket Engine 98
Vortex combustion in a hybrid rocket motor 97
Novel Activated Metal Powders for Improved Hybrid Fuels and Green Solid Propellants 95
A Comparative Study of the Aging Behavior of Different Nano-Sized Aluminum Powders 95
Hydrogen-Based Thrusters for Supersonic and Hypersonic Flight: Experimental Characterization 95
Nano-Sized and Mechanically Activated Composites: Perspectives for Enhanced Mass Burning Rate in Aluminized Solid Fuels for Hybrid Rocket Propulsion 94
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 91
Time-resolved regression rate of innovative hybrid solid fuel formulations 87
Comparison Between Nano-Sized Aluminum Powders with Different Coatings: Physical Analyses and Performance Test 86
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part II, Ballistic Characterization 85
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 84
Monte Carlo Analysis of a LEO Reentry Mission by Solid Rocket Propulsion 83
Aging Effects on Nano-Sized Aluminum Reactivity 83
Activated and Nano-Sized Aluminum as Metal Fuels in Solid Rocket Propellants 83
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Mechanical characterization 83
METODO PER LA LAVORAZIONE E/O L'ATTIVAZIONE MECCANICA DI POLVERI TRAMITE SFERE 79
Experimental evaluation of HTPB/paraffin fuel blends for hybrid rocket applications 77
Hybrid Propulsion System for Future Rocket Applications 73
Mapping of Aluminum Particle Dispersion in Solid Rocket Fuel Formulations 73
The FP7 Spartan Program Status and Achievements 70
Aggregation and Incipient Agglomeration in Metallized Solid Propellants and Solid Fuels for Rocket Propulsion 68
Cellular Structures for Solid Fuel Grain Reinforcement: Mechanical and Combustion Performance in Conventional and Non-Conventional Hybrid Rocket Engines 66
Coated Nano-Sized Aluminum Powders: Physical Analyses and Performance Tests in Hybrid Propulsion 65
Ignition and Combustion of HTPB-based Solid Fuels Loaded with Micron-sized Metals 64
Mechanically Activated Al/Mg Powders for Solid Rocket Propellants 64
Regression Rate Measurements in Lab-Scale Hybrid Burners 60
Regression Rate and CCPs Measurement of Metallized Solid Fuels 58
Liquefying Fuel Combustion in a Lab-scale Vortex Flow Pancake Hybrid Rocket Engine 57
Strategies for Paraffin-based Fuels Reinforcement: 3D Printing and Blending with Polymers 55
Anisotropy Effects in Hybrid Fuels Burning in a Microburner 54
Quasi-steady and Forced Transient Burning of a Vortex Flow Hybrid Motor 52
Impact of 3d-printing on the mechanical reinforcement and the ballistic response of paraffin-based fuels: The armored grain 52
End-To-end Flight Test for Planetary Landing, an Unprecedented Approach in Europe 51
Preparation and Characterization of Al/HTPB Composite for High Energetic Materials 47
Regression Rates and Anisotropy Effects in Hybrid Fuels Burning in a Microburner 46
Nanometric Powders Dispersion in a Polymeric Matrix 45
Development of a Compact Hybrid Rocket Engine for Low-Cost In-Space Propulsion 45
Thermite-For-Demise (T4D): Material Selection for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 44
Mixed-Hybrid Fuel Formulations: Composition, Regression Rate and Condensed Combustion Products 42
Reconstructed Ballistic Data Versus Wax Regression-Rate Intrusive Measurement in a Hybrid Rocket 42
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Ballistic characterization 39
Nano-Sized Bimetallic Aluminum-Copper Powders in HTPB-based Fuels 39
Ignition and combustion of hydroxyl-terminated polybutadiene (HTPB)-based solid fuels loaded with innovative micrometer-sized metals 37
Nickel acetylacetonate as decomposition catalyst for HTPB-based fuels: Regression rate enhancement effects 37
Nano-Sized Aluminum Powders as Energetic Additives for Hybrid Propulsion: Phisical Analysis and Performance Tests 36
Nano-sized Aluminum for Solid Fuel Regression Rate Enhancement 36
Space Debris Mitigation and Remediation: Perspectives of Affordable Hybrid Propulsion Implementations 36
Rheological and Mechanical Behavior of Coated Aluminum Loaded Nano-Composites 34
Towards High-Performing Paraffin-Based Fuels Exploiting the Armored Grain Concept 33
Lab-Scale Investigation of Metal Hydrides as Solid Fuel Additives for Hybrid Rocket Propulsion 30
Ballistic Characterization of Armored Grains with Vortex Flow Pancake Hybrid Rocket Engine 29
Thermite-for-Demise (T4D): Concept Definition for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 29
Thermite-for-Demise: Preliminary on-Ground Heat Transfer Experimental Testing 27
On the Statistics of Nanoaluminum Thermal Characterization and Its Correlation with the Slow Oxidation/Combustion Parameters 26
Development of Paraffin-Based Fuels for a Vortex Combustion Hybrid Rocket Engine 23
Numerical and experimental analysis of fuel regression rate in a lab-scale hybrid rocket engine with swirl injection 23
Test Activities on Hybrid Rocket Engines: Combustion Analyses and Green Storable Oxidizers - A Short Review 22
Effects of Vortex Flow Pancake Hybrid Rocket Engine Operating Parameters on Liquefying Fuel Combustion 19
Boosting Green Propellants: the Sustainable Armored Grain for Hybrid Rocket Propulsion 18
Numerical and Experimental Investigation of a Lab-Scale Paraffin Motor with Swirled Injection of Gaseous Oxygen 17
Paraffin-Based Fuels: Perspectives from Different Reinforcing Strategies and Metal Additives 16
Liquid Film Cooling: Advanced Modeling and Efforts Towards Validation 16
Thermite-for-Demise (T4D): Preliminary Assessment on the Effects of a Thermite Charge in Arc-Heated Wind Tunnel Experiments 15
Totale 8.449
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Categoria #
all - tutte 24.484
article - articoli 6.801
book - libri 0
conference - conferenze 15.039
curatela - curatele 0
other - altro 0
patent - brevetti 510
selected - selezionate 0
volume - volumi 2.134
Totale 48.968
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20202.112 0 0 171 139 380 372 250 182 210 94 204 110
2020/20211.332 105 103 95 82 84 196 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
2024/2025209 150 58 1 0 0 0 0 0 0 0 0 0
Totale 8.535