PAVARIN, DANIELE
 Distribuzione geografica
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Continente #
NA - Nord America 18.033
AS - Asia 12.181
EU - Europa 6.038
AF - Africa 2.012
SA - Sud America 1.900
OC - Oceania 184
Continente sconosciuto - Info sul continente non disponibili 78
Totale 40.426
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Nazione #
US - Stati Uniti d'America 17.008
SG - Singapore 3.753
CN - Cina 2.228
VN - Vietnam 1.766
IT - Italia 1.515
HK - Hong Kong 1.265
BR - Brasile 1.091
DE - Germania 649
FI - Finlandia 493
FR - Francia 487
IN - India 439
GB - Regno Unito 337
BD - Bangladesh 280
SE - Svezia 241
RU - Federazione Russa 225
NL - Olanda 222
UA - Ucraina 215
PL - Polonia 203
TR - Turchia 184
IQ - Iraq 180
CA - Canada 177
CI - Costa d'Avorio 177
JP - Giappone 173
AR - Argentina 162
BJ - Benin 133
PH - Filippine 128
PK - Pakistan 119
SA - Arabia Saudita 118
ES - Italia 115
ID - Indonesia 108
MX - Messico 103
EC - Ecuador 102
ZA - Sudafrica 101
KR - Corea 95
UZ - Uzbekistan 92
MA - Marocco 84
CO - Colombia 83
VE - Venezuela 81
CL - Cile 80
AE - Emirati Arabi Uniti 79
JO - Giordania 76
PY - Paraguay 75
IE - Irlanda 74
TH - Thailandia 73
IR - Iran 71
AZ - Azerbaigian 69
UY - Uruguay 69
AT - Austria 65
MY - Malesia 65
RO - Romania 64
TW - Taiwan 64
CH - Svizzera 63
IL - Israele 63
TN - Tunisia 63
KE - Kenya 60
SN - Senegal 60
DO - Repubblica Dominicana 59
PE - Perù 59
BY - Bielorussia 58
AU - Australia 57
DZ - Algeria 57
AO - Angola 56
LB - Libano 56
RS - Serbia 55
KZ - Kazakistan 54
NI - Nicaragua 54
PT - Portogallo 54
BO - Bolivia 53
MN - Mongolia 53
BA - Bosnia-Erzegovina 52
ET - Etiopia 51
HR - Croazia 51
EG - Egitto 49
JM - Giamaica 49
BB - Barbados 48
BE - Belgio 48
CZ - Repubblica Ceca 48
HU - Ungheria 48
LU - Lussemburgo 48
LY - Libia 48
MD - Moldavia 48
MZ - Mozambico 48
SI - Slovenia 48
BF - Burkina Faso 47
GA - Gabon 47
GN - Guinea 47
KG - Kirghizistan 47
NP - Nepal 47
AM - Armenia 46
MU - Mauritius 46
NO - Norvegia 46
SK - Slovacchia (Repubblica Slovacca) 46
TZ - Tanzania 46
AL - Albania 45
CR - Costa Rica 45
HT - Haiti 45
GE - Georgia 44
GR - Grecia 44
YT - Mayotte 44
BZ - Belize 43
Totale 38.349
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Città #
Singapore 2.141
San Jose 2.121
Ashburn 1.692
Fairfield 1.494
Chandler 1.275
Hong Kong 1.149
Woodbridge 896
Ann Arbor 755
Houston 663
Wilmington 615
Seattle 572
Jacksonville 564
Beijing 538
Cambridge 537
Ho Chi Minh City 525
Santa Clara 401
Hanoi 396
Boardman 369
Los Angeles 309
Princeton 278
New York 264
Lauterbourg 221
Helsinki 214
Medford 205
Abidjan 171
Padova 164
Munich 158
Roxbury 152
San Diego 141
Des Moines 134
Cotonou 131
Dong Ket 129
Milan 118
Bytom 116
Nanjing 114
São Paulo 109
Chicago 94
Rome 92
Turku 90
Buffalo 89
Da Nang 86
Guangzhou 86
Orem 84
Tokyo 83
Tashkent 79
Amman 72
Dallas 70
Haiphong 68
Baghdad 65
Frankfurt am Main 65
London 65
Baku 62
Dublin 58
Dakar 57
Montevideo 57
Montreal 56
Warsaw 56
Managua 53
Amsterdam 52
Chennai 52
Jeddah 52
Redondo Beach 52
Stockholm 50
Ulan Bator 50
Addis Ababa 48
Luanda 48
Nairobi 48
Vienna 46
Bridgetown 45
Bologna 44
Libreville 44
Toronto 44
Brooklyn 43
Hebei 43
Denver 42
Johannesburg 42
Shanghai 42
Conakry 41
Nanchang 41
Yerevan 41
Nouakchott 39
Rio de Janeiro 39
Hefei 38
Redwood City 38
Shenyang 38
Dar es Salaam 37
Harare 37
Lima 37
Bishkek 36
Maputo 36
Riga 36
Atlanta 35
Biên Hòa 35
Havana 35
Mumbai 35
Quito 35
Santiago 35
Bamako 34
Falkenstein 34
Kuala Lumpur 34
Totale 23.151
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Nome #
Novel magnetic inorganic composites: Synthesis and characterization 335
Design and In-orbit Demonstration of REGULUS, an Iodine electric propulsion system 314
REGULUS: A propulsion platform to boost small satellite missions 302
The "Vortex Reloaded" project: numerical investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 292
Comparative performance assessment of plasma reactors for the treatment of PFOA; reactor design, kinetics, mineralization and energy yield 280
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) 274
Analysis of transient vibrations on complex targets representing elementary configurations of GOCE satellite 262
Development and Test of an High Power RF Plasma Thruster in Project SAPERE-STRONG 261
Improvement of the CISAS high-shot-frequency light-gas gun 258
Development of a Counterbalanced Pendulum Thrust Stand for Electric Propulsion 258
Investigation of different strategies for access to space of small satellites on a defined LEO orbit 257
Off-line ionization tests using the surface and the plasma ion sources of the SPES project 256
CFD Simulation of a Hybrid Rocket Motor with Liquid Injection 255
Characterization and comparative evaluation of two atmospheric plasma sources for water treatment 254
Numerical Modeling of Paraffin-Based Fuels Behavior 252
Design and numerical characterization of a realistic plasma dipole 249
Helicon Plasma Hydrazine Combined Micro Project Overview and Development Status 248
Impact facility based upon high frequency two stage light-gas gun 248
Testing of a Long-Burning-Time Paraffin-Based Hybrid Rocket Motor 245
Numerical Model to Analyze Transient Behavior and Instabilities on Hybrid Rocket Motors 241
Scaling Parameters of Swirling Oxidizer Injection in Hybrid Rocket Motors 240
Real-Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor 239
Enhancement of microsatellites' mission capabilities: integration of REGULUS electric propulsion module into UniSat-7 237
Design and Testing of a 3D Printed 10 N Hydrogen Peroxide Monopropellant Thruster 235
A special design condition to increase the performance of two-stage light-gas guns 232
SPONGE: a Sounding Rocket Experiment for PMDs 232
Development of a Counterbalanced Pendulum Thrust Stand for Electric Propulsion 230
Hypervelocity experiments of impact cratering and catastrophic disruption of targets representative of minor bodies of the Solar System 229
Design and testing of a hydrogen peroxide bipropellant thruster 229
3D-VIRTUS: Equilibrium condition solver of radio-frequency magnetized plasma discharges for space applications 228
LISA: Mars and the limits of life 226
Acceleration fields induced by hypervelocity impacts on spacecraft structures 226
Development of a Flow Control Valve for a Throttleable Hybrid Rocket Motor and Throttling Fire Tests 222
Regression Rate Design Tailoring Through Vortex Injection in Hybrid Rocket Motors 221
E-REGULUS: development of a 150 W prototype of magnetically enhanced plasma thruster 219
Investigation of Effect of Diaphragms on the Efficiency of Hybrid Rockets 218
S.A.M., the Italian Martian Simulation Chamber 217
Active piston technique to optimize the chamber pressure in two-stage light-gas guns 215
A system to damp the free piston oscillations in a two-stage light-gas gun used for hypervelocity impact experiments 215
Update on green chemical propulsion activities and achievements by the University of Padua and its spin-off T4I 214
Curl plasma antenna for SATcom navigation systems 213
Numerical and Experimental Investigation on Vortex Injection in Hybrid Rocket Motors 212
A numerical model to analyze the transient behavior and instabilities on hybrid rocket motors 210
Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection - Part 2 207
Numerical model of the Plasma Source of a Helicon Plasma Thruster 206
ADVANCMENTS IN PLASMA ANTENNAS FOR SATCOM NAVIGATION SYSTEMS 205
Analysis of GOCE's disturbances induced by hypervelocity impact 204
The SPONGE rexus project: Overview of a sounding rocket experiment for PMDs 204
Numerical analyses of thermal protection design in hybrid rocket motors 204
REGULUS: Know-How Acquired on Iodine Propellant 203
REGULUS: INTEGRATION AND TESTING OF AN IODINE ELECTRIC PROPULSION SYSTEM 203
REGULUS: Iodine Fed Plasma Propulsion System for Small Satellites 202
Design of a thrust balance for RF plasma thruster characterization2014 IEEE Metrology for Aerospace (MetroAeroSpace) 201
Development and Testing of a Long Burning Time Lab-scale Paraffin-Based Hybrid Rocket Motor 201
Development and testing of an engineering model of a hydrogen peroxide based 1N propulsion unit 199
First experimental characterization of a gaseous plasma antenna in the UHF band 199
Numerical Investigation of Hybrid Motors for the EU FP7 SPARTAN Program 197
Design of a Hybrid Metal-Plasma Transmit-Array With Beam-Scanning Capabilities 196
Status and Achievements of the Hydrogen Peroxide Chemical Propulsion Research at Padua University 195
Antenna design and optimization for helicon plasma thruster with coupled surface and volume integral equations 194
Enhanced biDimensional pIc: an electrostatic/magnetostatic particle-in-cell code for plasma based systems 194
Feasibility study of a novel class of plasma antennas for SatCom navigation systems 194
Development of a Miniature Plasma Propulsion Module for Small Satellites 193
Numerical and Experimental Investigation of Unidirectional Vortex Injection in Hybrid Rocket Engines 193
Development and Flight Testing of a Hybrid Rocket Booster for UAV Assisted Take Off 190
Optimization of a H2O2 Gas Generator for a Hybrid Rocket Engine 189
Numerical Simulation of an Isochoric Combustion Chamber for Hybrid Rocket Propulsion 189
SPIREs: A Finite-Difference Frequency-Domain electromagnetic solver for inhomogeneous magnetized plasma cylinders 188
Fusion modeling approach for novel plasma sources 188
CFD Simulations of Self-Pressurized Nitrous Oxide Hybrid Rocket Motors 188
Acceleration fields induced by hypervelocity impacts on spacecraft structures" International Journal of Impact Engineering 187
Low Power RF Plasma Thruster Experimental Characterization 187
Design and Testing of a 3D Printed Regenerative Cooled Nozzle for a Hydrogen Peroxide based Bi-Propellant Thruster 187
Mini launcher vehicle University program Based on Hybrid propulsion 186
Swarm of lightsail nanosatellites for Solar System exploration 185
Computational Fluid Dynamics Simulation of Regression Rate in Hybrid Rockets 185
Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection 185
Experimental Characterization of a Hydrogen Peroxide Simulator 184
Impact of propulsion system characteristics on the potential for cost reduction of earth observation missions at very low altitudes 184
KEYNOTE: X-band Plasma-Based Reflective Surface 183
Feasibility study of medium power helicon thruster 183
Numerical Investigation of Hybrid Rocket Combustion Chamber Transient Behavior 181
Impact experiments on low-temperature bumpers 181
Ballistic Limit of CFRP Plates 180
Selecting materials to protect inflatable structures from the space environment 180
EUCLID satellite: Sloshing model development through computational fluid dynamics 180
S.A.M., the Italian Martian Simulation Chamber. 179
Active space debris removal by a hybrid propulsion module 179
Integrated approach for hybrid rocket technology development 179
A microwave interferometer for small and tenuous plasma density measurements 179
The "Vortex Reloaded" project: experimental investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 177
Study on the influence of the magnetic field geometry on the power deposition in a helicon plasma source 177
Feasibility Study for a Throttleable Hybrid Rocket Motor for Soft Landing 175
An estimation method for the Shock Response Spectrum propagating into plates subjected to hypervelocity impact 173
Project LANDAU: Boosting Plasma Antennas in Space 172
Explicit analytical equations for single port hybrid rocket combustion chamber sizing 171
Fusion modeling approach for novel plasma sources 171
An integral-equation approach to the analysis and design of plasma antennas 170
Numerical Suite for Gaseous Plasma Antennas Simulation 170
Experimental Characterization of a Plasma Dipole in the UHF band 169
Totale 21.205
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Categoria #
all - tutte 113.260
article - articoli 40.748
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 1.656
patent - brevetti 0
selected - selezionate 0
volume - volumi 277
Totale 155.941
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021291 0 0 0 0 0 0 0 0 0 0 0 291
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
2025/202621.070 820 1.650 2.665 3.261 2.336 917 2.653 2.117 2.166 1.294 839 352
Totale 40.693