PAVARIN, DANIELE
 Distribuzione geografica
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Continente #
NA - Nord America 14.084
AS - Asia 7.605
EU - Europa 4.955
AF - Africa 1.797
SA - Sud America 1.473
OC - Oceania 159
Continente sconosciuto - Info sul continente non disponibili 74
Totale 30.147
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Nazione #
US - Stati Uniti d'America 13.215
SG - Singapore 2.786
CN - Cina 1.416
IT - Italia 1.158
HK - Hong Kong 909
BR - Brasile 883
VN - Vietnam 618
DE - Germania 587
FI - Finlandia 431
GB - Regno Unito 253
SE - Svezia 230
FR - Francia 210
RU - Federazione Russa 203
UA - Ucraina 197
IN - India 192
PL - Polonia 187
NL - Olanda 185
CI - Costa d'Avorio 174
BJ - Benin 133
AR - Argentina 115
JP - Giappone 112
TR - Turchia 100
CA - Canada 97
ES - Italia 89
KR - Corea 82
MX - Messico 80
EC - Ecuador 70
IE - Irlanda 70
ID - Indonesia 69
IR - Iran 67
ZA - Sudafrica 64
IQ - Iraq 63
AE - Emirati Arabi Uniti 61
AZ - Azerbaigian 61
MA - Marocco 61
CH - Svizzera 59
PK - Pakistan 59
PY - Paraguay 59
UY - Uruguay 59
JO - Giordania 58
RO - Romania 57
CO - Colombia 56
DO - Repubblica Dominicana 55
AT - Austria 54
IL - Israele 54
SN - Senegal 54
BY - Bielorussia 53
AO - Angola 52
CL - Cile 50
MN - Mongolia 50
KZ - Kazakistan 49
TH - Thailandia 49
BA - Bosnia-Erzegovina 48
VE - Venezuela 48
GA - Gabon 47
HR - Croazia 47
LB - Libano 47
MZ - Mozambico 47
NI - Nicaragua 47
PE - Perù 47
SI - Slovenia 47
TN - Tunisia 47
BO - Bolivia 46
DZ - Algeria 46
JM - Giamaica 46
PT - Portogallo 46
TW - Taiwan 46
BB - Barbados 45
CZ - Repubblica Ceca 45
GN - Guinea 45
LU - Lussemburgo 45
LY - Libia 45
RS - Serbia 45
SK - Slovacchia (Repubblica Slovacca) 45
BE - Belgio 44
BF - Burkina Faso 44
HU - Ungheria 44
KG - Kirghizistan 44
MD - Moldavia 44
UZ - Uzbekistan 44
AM - Armenia 43
BD - Bangladesh 43
MY - Malesia 43
YT - Mayotte 43
AL - Albania 42
HT - Haiti 42
ME - Montenegro 42
MU - Mauritius 42
NO - Norvegia 42
TZ - Tanzania 42
KE - Kenya 41
MK - Macedonia 41
BZ - Belize 40
DK - Danimarca 40
BG - Bulgaria 39
CD - Congo 39
CR - Costa Rica 39
GE - Georgia 39
GR - Grecia 39
IS - Islanda 39
Totale 28.256
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Città #
Fairfield 1.494
Singapore 1.423
Chandler 1.275
Ashburn 1.230
Woodbridge 893
Hong Kong 859
Ann Arbor 755
Houston 647
Wilmington 613
Seattle 563
Jacksonville 562
Cambridge 537
Beijing 520
Santa Clara 378
Boardman 353
Princeton 277
Medford 204
Ho Chi Minh City 181
New York 175
Los Angeles 170
Abidjan 168
Padova 164
Helsinki 160
Munich 158
Roxbury 152
San Diego 138
Cotonou 131
Des Moines 129
Dong Ket 129
Bytom 116
Nanjing 114
Hanoi 100
São Paulo 91
Turku 90
Milan 78
Chicago 76
Buffalo 73
Rome 73
Amman 58
Baku 56
Dublin 54
Dakar 52
London 52
Redondo Beach 52
Dallas 49
Tokyo 49
Montevideo 48
Ulan Bator 48
Guangzhou 47
Managua 46
Libreville 44
Luanda 44
Hebei 43
Warsaw 43
Bridgetown 42
Stockholm 42
Vienna 41
Bologna 40
Conakry 40
Nanchang 40
Redwood City 38
Yerevan 38
Tashkent 37
Bishkek 36
Nouakchott 36
Shenyang 36
Hefei 35
Maputo 35
Bamako 34
Dar es Salaam 34
Falkenstein 34
Harare 34
Havana 33
Riga 33
Seoul 33
Vientiane 33
Castries 32
Kampala 32
Minsk 32
Montreal 32
Podgorica 32
Niamey 31
Noumea 31
Tbilisi 31
Tehran 31
Accra 30
Dushanbe 30
Lima 30
Ljubljana 30
Reykjavik 30
Salt Lake City 30
Brooklyn 29
Chennai 29
Denver 29
Kinshasa 29
Luxembourg 29
Nairobi 29
Ouagadougou 29
Phnom Penh 29
Praia 29
Totale 17.563
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Nome #
REGULUS: A propulsion platform to boost small satellite missions 238
The "Vortex Reloaded" project: numerical investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 234
Design and In-orbit Demonstration of REGULUS, an Iodine electric propulsion system 230
Characterization and comparative evaluation of two atmospheric plasma sources for water treatment 218
Comparative performance assessment of plasma reactors for the treatment of PFOA; reactor design, kinetics, mineralization and energy yield 218
Off-line ionization tests using the surface and the plasma ion sources of the SPES project 213
Development of a Counterbalanced Pendulum Thrust Stand for Electric Propulsion 211
Correction to: Design and Testing of a 3D Printed Regenerative Cooled Nozzle for a Hydrogen Peroxide based Bi-Propellant Thruster (AIAA Propulsion and Energy Forum, 2021) 211
Investigation of different strategies for access to space of small satellites on a defined LEO orbit 208
Helicon Plasma Hydrazine Combined Micro Project Overview and Development Status 202
Impact facility based upon high frequency two stage light-gas gun 200
Design and Testing of a 3D Printed 10 N Hydrogen Peroxide Monopropellant Thruster 199
Scaling Parameters of Swirling Oxidizer Injection in Hybrid Rocket Motors 198
Testing of a Long-Burning-Time Paraffin-Based Hybrid Rocket Motor 196
SPONGE: a Sounding Rocket Experiment for PMDs 193
Active piston technique to optimize the chamber pressure in two-stage light-gas guns 184
Analysis of transient vibrations on complex targets representing elementary configurations of GOCE satellite 184
Regression Rate Design Tailoring Through Vortex Injection in Hybrid Rocket Motors 183
A special design condition to increase the performance of two-stage light-gas guns 181
Development of a Counterbalanced Pendulum Thrust Stand for Electric Propulsion 181
Real-Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor 181
Numerical and Experimental Investigation on Vortex Injection in Hybrid Rocket Motors 178
Numerical Modeling of Paraffin-Based Fuels Behavior 178
Investigation of Effect of Diaphragms on the Efficiency of Hybrid Rockets 176
Hypervelocity experiments of impact cratering and catastrophic disruption of targets representative of minor bodies of the Solar System 175
CFD Simulation of a Hybrid Rocket Motor with Liquid Injection 175
Acceleration fields induced by hypervelocity impacts on spacecraft structures 174
S.A.M., the Italian Martian Simulation Chamber 174
Development of a Flow Control Valve for a Throttleable Hybrid Rocket Motor and Throttling Fire Tests 174
3D-VIRTUS: Equilibrium condition solver of radio-frequency magnetized plasma discharges for space applications 173
Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection - Part 2 171
The SPONGE rexus project: Overview of a sounding rocket experiment for PMDs 170
Development and Test of an High Power RF Plasma Thruster in Project SAPERE-STRONG 170
Improvement of the CISAS high-shot-frequency light-gas gun 169
Development and Testing of a Long Burning Time Lab-scale Paraffin-Based Hybrid Rocket Motor 169
E-REGULUS: development of a 150 W prototype of magnetically enhanced plasma thruster 167
A numerical model to analyze the transient behavior and instabilities on hybrid rocket motors 165
Numerical Model to Analyze Transient Behavior and Instabilities on Hybrid Rocket Motors 164
A system to damp the free piston oscillations in a two-stage light-gas gun used for hypervelocity impact experiments 163
First experimental characterization of a gaseous plasma antenna in the UHF band 163
Design and testing of a hydrogen peroxide bipropellant thruster 162
Novel magnetic inorganic composites: Synthesis and characterization 161
Enhancement of microsatellites' mission capabilities: integration of REGULUS electric propulsion module into UniSat-7 160
Acceleration fields induced by hypervelocity impacts on spacecraft structures" International Journal of Impact Engineering 159
CFD Simulations of Self-Pressurized Nitrous Oxide Hybrid Rocket Motors 159
Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection 158
Active space debris removal by a hybrid propulsion module 156
Computational Fluid Dynamics Simulation of Regression Rate in Hybrid Rockets 156
Design and numerical characterization of a realistic plasma dipole 156
Numerical analyses of thermal protection design in hybrid rocket motors 155
Low Power RF Plasma Thruster Experimental Characterization 154
Curl plasma antenna for SATcom navigation systems 154
Numerical Investigation of Hybrid Motors for the EU FP7 SPARTAN Program 154
Impact of propulsion system characteristics on the potential for cost reduction of earth observation missions at very low altitudes 154
Design of a Hybrid Metal-Plasma Transmit-Array With Beam-Scanning Capabilities 153
An estimation method for the Shock Response Spectrum propagating into plates subjected to hypervelocity impact 152
Optimization of a H2O2 Gas Generator for a Hybrid Rocket Engine 152
Enhanced biDimensional pIc: an electrostatic/magnetostatic particle-in-cell code for plasma based systems 152
Status and Achievements of the Hydrogen Peroxide Chemical Propulsion Research at Padua University 151
An integral-equation approach to the analysis and design of plasma antennas 150
LISA: Mars and the limits of life 149
S.A.M., the Italian Martian Simulation Chamber. 148
Feasibility study of medium power helicon thruster 148
The "Vortex Reloaded" project: experimental investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 148
Effect of hypervelocity impact on microcellular ceramic foams from a preceramic polymer 148
A microwave interferometer for small and tenuous plasma density measurements 147
Integrated approach for hybrid rocket technology development 146
REGULUS: Know-How Acquired on Iodine Propellant 146
Feasibility study of a novel class of plasma antennas for SatCom navigation systems 144
REGULUS: INTEGRATION AND TESTING OF AN IODINE ELECTRIC PROPULSION SYSTEM 144
Experimental Characterization of a Hydrogen Peroxide Simulator 142
Study on the influence of the magnetic field geometry on the power deposition in a helicon plasma source 142
Numerical Investigation of Hybrid Rocket Combustion Chamber Transient Behavior 141
Design of a thrust balance for RF plasma thruster characterization2014 IEEE Metrology for Aerospace (MetroAeroSpace) 141
Impact experiments on low-temperature bumpers 141
Mini launcher vehicle University program Based on Hybrid propulsion 140
Fusion modeling approach for novel plasma sources 140
ADVANCMENTS IN PLASMA ANTENNAS FOR SATCOM NAVIGATION SYSTEMS 140
SPIREs: A Finite-Difference Frequency-Domain electromagnetic solver for inhomogeneous magnetized plasma cylinders 139
Development and Flight Testing of a Hybrid Rocket Booster for UAV Assisted Take Off 139
EUCLID satellite: Sloshing model development through computational fluid dynamics 139
Numerical Simulation of an Isochoric Combustion Chamber for Hybrid Rocket Propulsion 139
Numerical and Experimental Investigation of Unidirectional Vortex Injection in Hybrid Rocket Engines 138
Thruster development set-up for the helicon plasma hydrazine combined micro research project 137
KEYNOTE: X-band Plasma-Based Reflective Surface 136
SPH evaluation of out-of-plane peak force transmitted during a hypervelocity impact 136
Selecting materials to protect inflatable structures from the space environment 135
Numerical Suite for Gaseous Plasma Antennas Simulation 135
Computational fluid dynamics simulation of hybrid rockets of different scales 134
Antenna design and optimization for helicon plasma thruster with coupled surface and volume integral equations 132
EUCLID satellite: Development of a lumped parameter model for sloshing description 132
Ray-tracing WKB analysis of Whistler waves in non-uniform magnetic fields applied to space thrusters 132
Explicit Analytical Equations for Single Port Hybrid Rocket Combustion Chamber Sizing 132
Design and Testing of a 3D Printed Regenerative Cooled Nozzle for a Hydrogen Peroxide based Bi-Propellant Thruster 132
Optimal low-thrust trajectory analysis for constant and variable specific impulse Thrusters generated by multi-objective evolutionary algorithms and nonlinear Programming 131
Feasibility Study for a Throttleable Hybrid Rocket Motor for Soft Landing 131
Application of Wavelet Transform to analyze acceleration signals generated by HVI on thin aluminum plates and all-aluminum honeycomb sandwich panels 128
Analysis of GOCE's disturbances induced by hypervelocity impact 128
Impact facility based upon high frequency two stage light-gas gun 128
Fusion modeling approach for novel plasma sources 128
Totale 16.155
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Categoria #
all - tutte 92.762
article - articoli 34.195
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 1.300
patent - brevetti 0
selected - selezionate 0
volume - volumi 225
Totale 128.482
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20211.608 0 0 0 0 0 195 52 239 335 187 309 291
2021/20222.306 49 328 185 102 145 128 66 216 161 114 197 615
2022/20232.609 470 287 65 300 397 347 9 193 298 48 144 51
2023/20241.391 73 175 120 124 55 191 101 98 80 83 127 164
2024/20255.789 45 450 254 316 664 198 229 530 552 203 952 1.396
2025/202610.786 820 1.650 2.665 3.261 2.336 54 0 0 0 0 0 0
Totale 30.409