PAVARIN, DANIELE
 Distribuzione geografica
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Continente #
NA - Nord America 10.408
EU - Europa 1.878
AS - Asia 988
OC - Oceania 11
AF - Africa 9
SA - Sud America 8
Continente sconosciuto - Info sul continente non disponibili 5
Totale 13.307
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Nazione #
US - Stati Uniti d'America 10.380
IT - Italia 753
CN - Cina 664
DE - Germania 275
FI - Finlandia 264
GB - Regno Unito 148
SE - Svezia 147
UA - Ucraina 139
VN - Vietnam 134
IN - India 84
IE - Irlanda 35
FR - Francia 34
CA - Canada 26
IR - Iran 25
NL - Olanda 23
JP - Giappone 20
ES - Italia 15
RO - Romania 14
SG - Singapore 13
HK - Hong Kong 11
KR - Corea 11
AU - Australia 9
BE - Belgio 7
TR - Turchia 6
RU - Federazione Russa 5
TW - Taiwan 5
AE - Emirati Arabi Uniti 4
CL - Cile 4
LB - Libano 4
PL - Polonia 4
AT - Austria 3
BR - Brasile 3
EG - Egitto 3
EU - Europa 3
LK - Sri Lanka 3
MY - Malesia 3
PT - Portogallo 3
A2 - ???statistics.table.value.countryCode.A2??? 2
HU - Ungheria 2
KE - Kenya 2
MX - Messico 2
NZ - Nuova Zelanda 2
UG - Uganda 2
BG - Bulgaria 1
BO - Bolivia 1
CH - Svizzera 1
CZ - Repubblica Ceca 1
DZ - Algeria 1
EE - Estonia 1
IQ - Iraq 1
LU - Lussemburgo 1
MA - Marocco 1
NO - Norvegia 1
SI - Slovenia 1
Totale 13.307
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Città #
Fairfield 1.494
Chandler 1.275
Woodbridge 893
Ann Arbor 755
Ashburn 684
Houston 636
Wilmington 606
Jacksonville 561
Seattle 556
Cambridge 537
Princeton 277
Beijing 250
Medford 204
Roxbury 152
San Diego 137
Dong Ket 129
Padova 128
Des Moines 127
Nanjing 113
Helsinki 109
New York 105
Boardman 100
Milan 47
Rome 44
Hebei 43
Guangzhou 41
Nanchang 40
Redwood City 38
Shenyang 35
Dublin 32
Ogden 28
London 24
Bologna 23
Norwalk 21
Napoli 17
Tehran 17
Changsha 16
Shanghai 16
Turin 16
Pune 15
Nürnberg 14
Tianjin 14
Jiaxing 13
Jinan 13
Costabissara 11
Tokyo 9
Dallas 8
Falls Church 8
Romano di Lombardia 8
Stigliano 8
Verona 8
Washington 8
Bonndorf 7
Chennai 7
Hangzhou 7
Kunming 7
Leeds 7
Southend 7
Torino 7
Hong Kong 6
Kharkiv 6
Lodi 6
Manchester 6
Munich 6
Naples 6
Rimini 6
Ahmedabad 5
Borås 5
Brussels 5
Chengdu 5
Haikou 5
Hefei 5
Hounslow 5
Imola 5
Indiana 5
Montreuil 5
Ottawa 5
Paris 5
Selvazzano Dentro 5
Tappahannock 5
Thierhaupten 5
Toronto 5
Venezia 5
Vicenza 5
Abu Dhabi 4
Belluno 4
Brugherio 4
Cagliari 4
Centro 4
Guildford 4
Lanzhou 4
Lappeenranta 4
Los Altos 4
Madrid 4
Sant'elena 4
Venice 4
Xi'an 4
A Coruña 3
Amsterdam 3
Arroyo Grande 3
Totale 10.705
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Nome #
The "Vortex Reloaded" project: numerical investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 171
Characterization and comparative evaluation of two atmospheric plasma sources for water treatment 144
Off-line ionization tests using the surface and the plasma ion sources of the SPES project 130
Impact facility based upon high frequency two stage light-gas gun 129
Helicon Plasma Hydrazine Combined Micro Project Overview and Development Status 121
Scaling Parameters of Swirling Oxidizer Injection in Hybrid Rocket Motors 119
REGULUS: A propulsion platform to boost small satellite missions 116
Development of a Counterbalanced Pendulum Thrust Stand for Electric Propulsion 115
A system to damp the free piston oscillations in a two-stage light-gas gun used for hypervelocity impact experiments 114
Hypervelocity experiments of impact cratering and catastrophic disruption of targets representative of minor bodies of the Solar System 112
Design and Testing of a 3D Printed 10 N Hydrogen Peroxide Monopropellant Thruster 112
A special design condition to increase the performance of two-stage light-gas guns 111
Real-Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor 110
Active piston technique to optimize the chamber pressure in two-stage light-gas guns 108
Analysis of transient vibrations on complex targets representing elementary configurations of GOCE satellite 107
S.A.M., the Italian Martian Simulation Chamber 107
Comparative performance assessment of plasma reactors for the treatment of PFOA; reactor design, kinetics, mineralization and energy yield 107
Testing of a Long-Burning-Time Paraffin-Based Hybrid Rocket Motor 105
Regression Rate Design Tailoring Through Vortex Injection in Hybrid Rocket Motors 102
Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection - Part 2 100
Development of a Flow Control Valve for a Throttleable Hybrid Rocket Motor and Throttling Fire Tests 100
Acceleration fields induced by hypervelocity impacts on spacecraft structures" International Journal of Impact Engineering 99
Active space debris removal by a hybrid propulsion module 99
Design and In-orbit Demonstration of REGULUS, an Iodine electric propulsion system 99
Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection 97
Numerical and Experimental Investigation on Vortex Injection in Hybrid Rocket Motors 96
Acceleration fields induced by hypervelocity impacts on spacecraft structures 96
Effect of hypervelocity impact on microcellular ceramic foams from a preceramic polymer 96
CFD Simulation of a Hybrid Rocket Motor with Liquid Injection 95
Development and Testing of a Long Burning Time Lab-scale Paraffin-Based Hybrid Rocket Motor 95
SPH evaluation of out-of-plane peak force transmitted during a hypervelocity impact 94
Improvement of the CISAS high-shot-frequency light-gas gun 92
An estimation method for the Shock Response Spectrum propagating into plates subjected to hypervelocity impact 92
Investigation of Effect of Diaphragms on the Efficiency of Hybrid Rockets 91
An integral-equation approach to the analysis and design of plasma antennas 91
A microwave interferometer for small and tenuous plasma density measurements 90
S.A.M., the Italian Martian Simulation Chamber. 89
Selecting materials to protect inflatable structures from the space environment 88
Computational Fluid Dynamics Simulation of Regression Rate in Hybrid Rockets 88
A numerical model to analyze the transient behavior and instabilities on hybrid rocket motors 88
Numerical Modeling of Paraffin-Based Fuels Behavior 88
Ray-tracing WKB analysis of Whistler waves in non-uniform magnetic fields applied to space thrusters 87
Impact experiments on low-temperature bumpers 87
CFD Simulations of Self-Pressurized Nitrous Oxide Hybrid Rocket Motors 87
Antenna design and optimization for helicon plasma thruster with coupled surface and volume integral equations 85
Numerical Model to Analyze Transient Behavior and Instabilities on Hybrid Rocket Motors 85
Application of Wavelet Transform to analyze acceleration signals generated by HVI on thin aluminum plates and all-aluminum honeycomb sandwich panels 84
Development of a Counterbalanced Pendulum Thrust Stand for Electric Propulsion 84
SPONGE: a Sounding Rocket Experiment for PMDs 84
Numerical Investigation of Hybrid Motors for the EU FP7 SPARTAN Program 84
Low Power RF Plasma Thruster Experimental Characterization 83
Fusion modeling approach for novel plasma sources 83
Performance Analysis of a Medium- Power Helicon Thruster 80
3D-VIRTUS: Equilibrium condition solver of radio-frequency magnetized plasma discharges for space applications 80
Impact of propulsion system characteristics on the potential for cost reduction of earth observation missions at very low altitudes 80
Numerical simulation of the Helicon Double Layer Thruster concept 79
LISA: Mars and the limits of life 79
Impact facility based upon high frequency two stage light-gas gun. 78
Development and Test of an High Power RF Plasma Thruster in Project SAPERE-STRONG 77
Feasibility study of medium power helicon thruster 76
Fusion modeling approach for novel plasma sources 76
Debris Impact on CFRP-AL Honeycomb Sandwich Structure 75
Testing and CFD Simulation of Diaphragm Hybrid Rocket Motors 75
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) 75
Implicitly charge-conserving solver for Boltzmann electrons 74
Impact facility based upon high frequency two stage light-gas gun 74
Large debris removal mission in LEO based on hybrid propulsion 74
Ballistic Limit of CFRP Plates 73
Optimization of a H2O2 Gas Generator for a Hybrid Rocket Engine 73
Numerical Investigation of Hybrid Rocket Combustion Chamber Transient Behavior 73
Enhanced biDimensional pIc: an electrostatic/magnetostatic particle-in-cell code for plasma based systems 73
Enhancement of microsatellites' mission capabilities: integration of REGULUS electric propulsion module into UniSat-7 73
Diagnostic Procedure for two stage light gas gun pellet injector 72
Design of a thrust balance for RF plasma thruster characterization2014 IEEE Metrology for Aerospace (MetroAeroSpace) 72
The SPONGE rexus project: Overview of a sounding rocket experiment for PMDs 72
Integrated approach for hybrid rocket technology development 72
ORNL Mock-up tests of Inside Launch Pellet Injection on JET and LHD 72
Mini launcher vehicle University program Based on Hybrid propulsion 71
The "Vortex Reloaded" project: experimental investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 71
EUCLID satellite: Sloshing model development through computational fluid dynamics 70
Explicit Analytical Equations for Single Port Hybrid Rocket Combustion Chamber Sizing 70
Design and numerical characterization of a realistic plasma dipole 70
SPIREs: A Finite-Difference Frequency-Domain electromagnetic solver for inhomogeneous magnetized plasma cylinders 69
Testing and CFD simulation of diaphragm hybrid rocket motors 69
Numerical and Experimental Investigation of Unidirectional Vortex Injection in Hybrid Rocket Engines 69
Study on the influence of the magnetic field geometry on the power deposition in a helicon plasma source 69
First experimental characterization of a gaseous plasma antenna in the UHF band 68
Status and Achievements of the Hydrogen Peroxide Chemical Propulsion Research at Padua University 68
Generation of transient vibrations on aluminum honeycomb sandwich panels subjected to hypervelocity impacts 68
Multi-objective low-thrust trajectory optimisation: Variable and constant specific impulse 67
Collision-Avoidance Maneuvers for a satellite Pair Flying in Tight Formation 67
Controlled Orbital Dynamics of Low Altitude Formations by means of Electric Propulsion 65
Optimal low-thrust trajectory analysis for constant and variable specific impulse thrusters generated by multi-objective evolutionary algorithms and nonlinear programming 64
Optimal low-thrust trajectory analysis for constant and variable specific impulse Thrusters generated by multi-objective evolutionary algorithms and nonlinear Programming 64
Off-Line Ionization Tests Using the Surface and Plasma Ion Sources of the SPES Project 64
Thruster development set-up for the helicon plasma hydrazine combined micro research project 63
Analytic Wave Solution with Helicon and Trivelpiece-Gould Modes in an Annular Plasma 63
Numerical Simulation of an Isochoric Combustion Chamber for Hybrid Rocket Propulsion 63
Numerical analyses of thermal protection design in hybrid rocket motors 63
Radiofrequency Plasma Thrusters: Modelling Of Ion Cyclotron Resonance Heating And System Performance 61
Totale 8.649
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Categoria #
all - tutte 45.098
article - articoli 18.456
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 593
patent - brevetti 0
selected - selezionate 0
volume - volumi 100
Totale 64.247
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019710 0 0 0 0 0 0 0 0 0 169 295 246
2019/20202.668 356 59 67 210 259 197 250 299 270 311 281 109
2020/20212.538 76 119 65 237 433 195 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
2023/20241.071 73 175 120 124 55 191 101 98 80 54 0 0
Totale 13.514