ANDRENUCCI, MARIANO
 Distribuzione geografica
Continente #
NA - Nord America 13.201
AS - Asia 6.947
EU - Europa 5.944
SA - Sud America 734
AF - Africa 216
OC - Oceania 34
Continente sconosciuto - Info sul continente non disponibili 5
Totale 27.081
Nazione #
US - Stati Uniti d'America 12.769
IT - Italia 2.215
CN - Cina 2.048
SG - Singapore 1.900
HK - Hong Kong 1.275
SE - Svezia 778
BR - Brasile 624
DE - Germania 610
VN - Vietnam 464
BG - Bulgaria 461
KR - Corea 416
UA - Ucraina 416
CA - Canada 388
RU - Federazione Russa 277
TR - Turchia 277
FR - Francia 275
GB - Regno Unito 271
FI - Finlandia 254
CH - Svizzera 194
IN - India 144
JP - Giappone 132
CI - Costa d'Avorio 102
ES - Italia 46
IR - Iran 44
NL - Olanda 38
AR - Argentina 32
BD - Bangladesh 31
IQ - Iraq 29
AU - Australia 25
MX - Messico 25
SN - Senegal 25
PK - Pakistan 24
ZA - Sudafrica 24
BE - Belgio 23
CO - Colombia 22
AT - Austria 21
EC - Ecuador 18
ID - Indonesia 17
IL - Israele 15
MY - Malesia 15
SA - Arabia Saudita 14
CZ - Repubblica Ceca 13
MA - Marocco 13
AE - Emirati Arabi Uniti 12
DZ - Algeria 12
UZ - Uzbekistan 12
KE - Kenya 11
PL - Polonia 11
TH - Thailandia 11
TW - Taiwan 11
VE - Venezuela 11
PH - Filippine 10
EG - Egitto 9
NZ - Nuova Zelanda 8
PY - Paraguay 8
RO - Romania 8
BJ - Benin 7
GR - Grecia 7
JM - Giamaica 7
PE - Perù 7
EU - Europa 5
JO - Giordania 5
OM - Oman 5
BO - Bolivia 4
BY - Bielorussia 4
GE - Georgia 4
IE - Irlanda 4
KZ - Kazakistan 4
TN - Tunisia 4
UY - Uruguay 4
AZ - Azerbaigian 3
CL - Cile 3
DO - Repubblica Dominicana 3
KW - Kuwait 3
LK - Sri Lanka 3
PS - Palestinian Territory 3
SK - Slovacchia (Repubblica Slovacca) 3
TT - Trinidad e Tobago 3
ET - Etiopia 2
KG - Kirghizistan 2
LB - Libano 2
LT - Lituania 2
LV - Lettonia 2
LY - Libia 2
MD - Moldavia 2
MN - Mongolia 2
MO - Macao, regione amministrativa speciale della Cina 2
MV - Maldive 2
NG - Nigeria 2
NP - Nepal 2
PT - Portogallo 2
RS - Serbia 2
AM - Armenia 1
BA - Bosnia-Erzegovina 1
BH - Bahrain 1
CR - Costa Rica 1
DK - Danimarca 1
EE - Estonia 1
FJ - Figi 1
GD - Grenada 1
Totale 27.069
Città #
Woodbridge 1.755
Ann Arbor 1.358
Hong Kong 1.219
Singapore 1.080
Ashburn 1.020
Houston 1.010
Milan 833
Chandler 826
Fairfield 746
Santa Clara 612
Jacksonville 596
San Jose 480
Sofia 460
Beijing 398
Ottawa 365
Wilmington 361
Shanghai 342
Dallas 340
Hefei 328
Seoul 323
New York 308
Seattle 289
Cambridge 261
Boardman 232
Nanjing 197
Bern 189
Princeton 185
Lawrence 181
Izmir 161
Lauterbourg 153
Rome 128
Los Angeles 118
Des Moines 113
Dearborn 103
Jüchen 103
Abidjan 102
Ho Chi Minh City 102
Frankfurt am Main 98
Tokyo 86
Medford 84
Hanoi 82
Serra 82
Florence 79
Istanbul 78
Buffalo 76
Helsinki 71
Nanchang 69
Dong Ket 65
Pisa 62
Redwood City 56
Kunming 53
Boulder 52
Redondo Beach 49
Changsha 45
Düsseldorf 42
São Paulo 42
Council Bluffs 37
Livorno 33
Hebei 32
Shenyang 32
Ogden 29
Falls Church 28
Munich 28
Jiaxing 27
Chennai 25
Dakar 25
San Diego 25
Central 24
Norwalk 24
Brussels 22
Hangzhou 22
Madrid 22
Rio de Janeiro 22
Atlanta 21
London 21
Orem 21
Marseille 20
Columbus 19
Daejeon 19
Fuzhou 18
Lucca 18
The Dalles 17
Pune 16
Tianjin 16
Naples 15
Stockholm 15
Auburn Hills 14
Belo Horizonte 14
Da Nang 14
Indiana 14
New Delhi 14
Orange 14
Phoenix 14
Turin 14
Yuseong-gu 14
Brasília 13
Moscow 13
San Francisco 13
Johannesburg 12
Manchester 12
Totale 19.530
Nome #
Development of a LaB6 cathode for high-power Hall thrusters 332
Recent Advances in Hall Thruster Scaling Methodology 251
L’impiego dei propulsori ad emissione di campo (FEEP) per missioni a bassissima spinta 235
Sitael Hollow Cathodes for Low-Power Hall Effect Thrusters 235
Recent Advances in Low-Current Hollow Cathodes at SITAEL 224
Development and Characterization of a Pulsed Plasma Thruster 216
Low-Thrust Maneuvers for the Efficient Modification of Orbital Elements 215
Development Status of SITAEL’s 20 kW Class Hall Thruster 210
Performance of Centrospazio Hypersonic High Enthalpy Wind Tunnel 207
Overview of Hollow Cathodes Development at Sitael 205
FEEP Thruster Plume Investigation with Langmuir Probes 200
Giannini, Ducati and the Dawn of MPD Propulsion 196
Earth-Mars Halo to Halo Low Thrust Manifold Transfers 196
Centrospazio Progress on MPDT Hollow Cathodes 194
A Hollow Cathode Model for Application to Electric Propulsion 189
Exploitation of Three-Body Dynamics by Electric Propulsion for Outer Planetary Missions 189
Advanced scaling model for simplified thrust and power scaling of an applied-field magnetoplasmadynamic thruster 188
Galileo Galilei: Flight Experiment on the Equivalence Principle with Field Emission Electric Propulsion 188
Hollow Cathodes for Low-Power Hall Effect Thrusters 187
Low-Current Hollow Cathodes for Hall Effect Thrusters 187
Experimental Study of FEEP Emitter Starting Characteristics 186
Attitude and Orbit Control of Small Satellites and Constellations with FEEP Thrusters 186
Amplifying and Evanescent Waves in Hall Thrusters 186
Modeling of LaB6 hollow cathode performance and lifetime 186
A Flight Demonstration of FEEP: Electric Thrusters for Microgravity Laboratories and Drag-Free Spacecraft 185
A Hollow Cathode Model for Application to the Electric Propulsion 185
Plasma plume diagnostics of a LaB6 hollow cathode with triple Langmuir probes 184
A Large Space Simulator for Electric Propulsion Testing: Design Requirements and Engineering Analysis 183
Experimental Investigation of a Plasma Bridge Neutralizer for a mN FEEP Thruster 182
Arcjet Propulsion System Study for NSSK 182
Space-Borne Astronomical Gravity-Wave Interferometer Mission (SAGITTARIUS): The Field Emission Electric Propulsion Option 182
Field Emission Electric Propulsion (FEEP) System Study 181
Time-Resolved Plasma Diagnostic by Laser-Diode Spectroscopy 181
Experimental Behavior of FEEP Emitters Fed by a Caesium Chromate Tank 179
Qualification Status of the FEEP-150 Electric Micropropulsion Subsystem 179
100-hr Endurance Test on a Tungsten Multi-rod Hollow Cathode for MPD Thrusters 179
Development of a Numerical Model of the Nozzle Flow in Low Power Arcjet Thrusters 178
Further Experimental Evidences of the Development of Kink Instabilities in MPD Thrusters 176
Preliminary Design of a 25 kW HET 176
Turbulence Measurements in a 100 W Hall Thruster 175
Electron Dynamics in Hall Thrusters 175
Fundamental Scaling Laws for Electric Propulsion Concepts - Part 2: MPD Thrusters 174
Mission Analysis and Architecture Definition for a Small Electric Propulsion Transfer Module to the Moon 174
Triple Langmuir Probes Measurements of LaB6 Hollow Cathodes Plume 174
Experimental Performance of Continuous and Pulsed FEEP Thrusters 173
A [Re(Re-)] Examination of Electron Motion in Hall Thruster Fields 173
Three Body Invariant Manifold Transition with Electric Propulsion 173
Ion Beam Modeling in FEEP Thrusters 172
One Millinewton FEEP Thruster Tests 172
A Large Space Simulator for Electric Propulsion Testing: Design Requirements and Engineering Analysis 172
FEEP Thruster Performance at High Background Pressure 170
Tunable Diode Laser Absorption for Argon Plasma Produced in an MPD Thruster 169
Fundamental Scaling Laws for Electric Propulsion Concepts –Part 2: MPD Thrusters 169
Development Status of the HT-100 Miniaturized Hall Effect Thruster System 169
Radioisotope Low-Power Electric Propulsion Missions to the Outer Planets 169
Development of a LaB6 Cathode for High-Power Hall Thrusters 169
Galileo Galilei''. Flight Experiment on the Equivalence Principle with Field Emission Electric Propulsion. GG-FEEP2, In "Small and Medium Size Italian Scientific Satellites 168
Control Strategies for Orbit Maintenance of LEO Small Satellites With FEEP 168
FEEP Thrusters: Development Status and Prospects 167
Magnetoplasmadynamic Thrusters 167
Performance of an Applied Field MPD Thruster with a Pre-ionization Chamber 166
Low-frequency cathode plume oscillations in a 5-30A LaB6 cathode 166
Cost Effective Electric Propulsion Missions to the Outer Planets 165
A scaling methodology for high-power magnetically shielded Hall thrusters 165
GG Drag Compensation with FEEP Thrusters 164
A 3D model for MFD flow simulation 164
A VEGA Dedicated Electric Propulsion Transfer Module To The Moon 164
HET Scaling Methodology: Improvement and Assessment 164
Development of Hollow Cathodes for Space Electric Propulsion at Sitael 164
Magneto-Plasma-Dynamic Thrusters for Space Applications 163
MPD Thruster Plume Diagnostics 159
Simulazioni d’Impatto in Manovre di Rendez-Vous 159
Fundamental Scaling Laws for Electric Propulsion Concepts - Part I: Hall Effect Thrusters 159
3-D Plume Characterization of a FEEP Thruster 159
An Improved Hall Thruster Scaling Methodology 158
Development of Hollow Cathodes for 5 to 20 kW Hall Thrusters 158
Kink Instabilities in a Magneto-Plasma-Dynamic Thruster With and Without External Magnetic Field 156
Hall Thrusters Design and Optimization 156
Experimental Investigation of Magnetohydrodynamic Instabilities in a Magneto-Plasma-Dynamic Thruster 155
Experimental Performance of a Low Power Neutralizer for a Micronewton FEEP Thruster 155
3-D Plume Characterization of a FEEP Thruster 155
Further Experimental Evidences of the Development of Kink Instabilities in MPD Thrusters 154
Three Body Invariant Manifold Transition with Electric Propulsion 153
PIC/DSMC Models for Hall Effect Thruster Plumes: Present Status and Ways Forward 149
Unsteady Ballistic Code for Performance Prediction of Solid Propellant Rocket Engines 149
Experimental Performance of Field Emission Microthrusters 149
Power Constrained Uranus Transfer and Moons Tour by Three Body Invariant Manifolds and Electric Propulsion 148
Filamentation Instability and Onset in MPD Thrusters 147
FEEP Microthruster Technology Status and Potential Applications 146
Trajectory Design Considerations and Computational Tools for Electric Propulsion Missions 146
Experimental Characterization of a LaB6 Hollow Cathode for Low-Power Hall Effect Thrusters 144
Development of a Telemicroscopy Diagnostic Apparatus and Erosion Modelling in Hall Effect Thrusters 143
Victor B. Tikhonov's MHD Channel Theory: A Review 141
Spontaneous Symmetry Breaking in MPD Plasmas 141
3D Model Developments for Aerospace Applications 140
New Developments in Applied Field MPD Thrusters 139
Centrospazio Progress on MPDT Hollow Cathodes 139
FEEP Thruster Survivability in the LEO Atomic Oxygen Environment 139
null 138
Experimental study of a Multichannel Hollow Cathode for High Power MPD Thrusters 136
Totale 17.407
Categoria #
all - tutte 64.970
article - articoli 0
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 64.970


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021323 0 0 0 0 0 0 0 0 0 0 79 244
2021/20221.721 6 163 43 114 360 286 31 69 109 31 78 431
2022/20232.301 256 221 132 216 272 339 27 176 477 36 123 26
2023/20242.457 443 369 320 206 346 334 48 41 50 44 79 177
2024/20255.086 70 237 101 271 429 462 458 344 576 728 565 845
2025/20264.752 298 725 510 312 530 540 800 229 296 504 8 0
Totale 27.265