CINECA IRIS Institutional Research Information System

ANDRENUCCI, MARIANO
 Distribuzione geografica
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Continente #
NA - Nord America 10.447
EU - Europa 4.992
AS - Asia 1.951
AF - Africa 145
OC - Oceania 24
SA - Sud America 14
Continente sconosciuto - Info sul continente non disponibili 5
Totale 17.578
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Nazione #
US - Stati Uniti d'America 10.071
IT - Italia 1.960
CN - Cina 971
SE - Svezia 774
DE - Germania 525
BG - Bulgaria 461
UA - Ucraina 407
CA - Canada 374
SG - Singapore 217
GB - Regno Unito 195
CH - Svizzera 192
VN - Vietnam 187
TR - Turchia 181
FI - Finlandia 175
RU - Federazione Russa 101
CI - Costa d'Avorio 100
KR - Corea 100
HK - Hong Kong 85
FR - Francia 78
IN - India 69
JP - Giappone 38
IR - Iran 32
ES - Italia 30
BE - Belgio 23
SN - Senegal 22
AU - Australia 18
AT - Austria 17
NL - Olanda 14
CZ - Repubblica Ceca 12
PK - Pakistan 12
TH - Thailandia 10
IL - Israele 9
TW - Taiwan 9
BJ - Benin 7
DZ - Algeria 7
GR - Grecia 7
NZ - Nuova Zelanda 6
AE - Emirati Arabi Uniti 5
BR - Brasile 5
CO - Colombia 5
EU - Europa 5
ID - Indonesia 5
RO - Romania 5
EG - Egitto 4
PL - Polonia 4
LK - Sri Lanka 3
MY - Malesia 3
SK - Slovacchia (Repubblica Slovacca) 3
AR - Argentina 2
GE - Georgia 2
KW - Kuwait 2
MN - Mongolia 2
MO - Macao, regione amministrativa speciale della Cina 2
MX - Messico 2
NG - Nigeria 2
PT - Portogallo 2
AZ - Azerbaigian 1
BA - Bosnia-Erzegovina 1
BY - Bielorussia 1
DK - Danimarca 1
EC - Ecuador 1
HU - Ungheria 1
IE - Irlanda 1
KZ - Kazakistan 1
MD - Moldavia 1
OM - Oman 1
PH - Filippine 1
QA - Qatar 1
RS - Serbia 1
SA - Arabia Saudita 1
SC - Seychelles 1
TN - Tunisia 1
TZ - Tanzania 1
UZ - Uzbekistan 1
VE - Venezuela 1
Totale 17.578
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Città #
Woodbridge 1.755
Ann Arbor 1.356
Houston 1.008
Chandler 826
Milan 811
Fairfield 746
Jacksonville 596
Sofia 460
Ottawa 364
Wilmington 358
Ashburn 351
Beijing 325
New York 290
Seattle 286
Cambridge 261
Boardman 230
Nanjing 195
Bern 189
Princeton 185
Lawrence 181
Izmir 161
Des Moines 111
Singapore 106
Dearborn 103
Jüchen 103
Abidjan 100
Rome 92
Medford 84
Serra 81
Frankfurt am Main 69
Nanchang 68
Dong Ket 65
Florence 59
Redwood City 56
Boulder 52
Kunming 51
Changsha 42
Hong Kong 40
Los Angeles 40
Düsseldorf 34
Hebei 32
Seoul 30
Ogden 29
Falls Church 28
Livorno 28
Shenyang 28
Jiaxing 27
San Diego 25
Central 24
Norwalk 24
Brussels 22
Dakar 22
Pisa 22
Hangzhou 20
Hefei 20
Marseille 19
Daejeon 17
Madrid 16
Shanghai 15
Auburn Hills 14
Indiana 14
Orange 14
Tianjin 14
Karachi 11
Moscow 11
Pune 11
Stockholm 11
Anagni 10
San Francisco 10
London 9
Nürnberg 9
Yuseong-gu 9
Central District 8
Forte Dei Marmi 8
Guangzhou 8
Lucca 8
Melbourne 8
New Delhi 8
Padova 8
Tappahannock 8
Verona 8
Bremen 7
Cotonou 7
Grafing 7
Harbin 7
Jinan 7
Kent 7
Mangalore 7
Tokyo 7
Washington 7
Zhengzhou 7
Beaverton 6
Changchun 6
Kocaeli 6
Lanzhou 6
Mapo-gu 6
Santa Clara 6
Smyrna 6
Southampton 6
Torino 6
Totale 13.081
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Nome #
Development of a LaB6 cathode for high-power Hall thrusters 256
L’impiego dei propulsori ad emissione di campo (FEEP) per missioni a bassissima spinta 153
A Large Space Simulator for Electric Propulsion Testing: Design Requirements and Engineering Analysis 147
Amplifying and Evanescent Waves in Hall Thrusters 146
Centrospazio Progress on MPDT Hollow Cathodes 145
Giannini, Ducati and the Dawn of MPD Propulsion 144
FEEP Thruster Plume Investigation with Langmuir Probes 142
Earth-Mars Halo to Halo Low Thrust Manifold Transfers 141
Exploitation of Three-Body Dynamics by Electric Propulsion for Outer Planetary Missions 139
null 138
Advanced scaling model for simplified thrust and power scaling of an applied-field magnetoplasmadynamic thruster 136
A Hollow Cathode Model for Application to Electric Propulsion 135
Mission Analysis and Architecture Definition for a Small Electric Propulsion Transfer Module to the Moon 135
Turbulence Measurements in a 100 W Hall Thruster 135
Electron Dynamics in Hall Thrusters 135
Qualification Status of the FEEP-150 Electric Micropropulsion Subsystem 134
A Hollow Cathode Model for Application to the Electric Propulsion 133
null 132
Three Body Invariant Manifold Transition with Electric Propulsion 132
Modeling of LaB6 hollow cathode performance and lifetime 132
Preliminary Design of a 25 kW HET 130
Galileo Galilei: Flight Experiment on the Equivalence Principle with Field Emission Electric Propulsion 130
Performance of Centrospazio Hypersonic High Enthalpy Wind Tunnel 129
Attitude and Orbit Control of Small Satellites and Constellations with FEEP Thrusters 129
Fundamental Scaling Laws for Electric Propulsion Concepts - Part 2: MPD Thrusters 128
Cost Effective Electric Propulsion Missions to the Outer Planets 128
Low-Thrust Maneuvers for the Efficient Modification of Orbital Elements 128
Fundamental Scaling Laws for Electric Propulsion Concepts –Part 2: MPD Thrusters 127
Radioisotope Low-Power Electric Propulsion Missions to the Outer Planets 127
100-hr Endurance Test on a Tungsten Multi-rod Hollow Cathode for MPD Thrusters 127
Further Experimental Evidences of the Development of Kink Instabilities in MPD Thrusters 126
A [Re(Re-)] Examination of Electron Motion in Hall Thruster Fields 126
Overview of Hollow Cathodes Development at Sitael 126
Development Status of SITAEL’s 20 kW Class Hall Thruster 126
3-D Plume Characterization of a FEEP Thruster 126
Experimental Behavior of FEEP Emitters Fed by a Caesium Chromate Tank 125
Field Emission Electric Propulsion (FEEP) System Study 124
Development and Characterization of a Pulsed Plasma Thruster 124
Time-Resolved Plasma Diagnostic by Laser-Diode Spectroscopy 124
Control Strategies for Orbit Maintenance of LEO Small Satellites With FEEP 123
3-D Plume Characterization of a FEEP Thruster 123
null 123
null 123
A Flight Demonstration of FEEP: Electric Thrusters for Microgravity Laboratories and Drag-Free Spacecraft 122
null 122
Development Status of the HT-100 Miniaturized Hall Effect Thruster System 121
HET Scaling Methodology: Improvement and Assessment 121
Arcjet Propulsion System Study for NSSK 119
An Improved Hall Thruster Scaling Methodology 119
A VEGA Dedicated Electric Propulsion Transfer Module To The Moon 119
Space-Borne Astronomical Gravity-Wave Interferometer Mission (SAGITTARIUS): The Field Emission Electric Propulsion Option 117
Hall Thrusters Design and Optimization 117
null 117
A Large Space Simulator for Electric Propulsion Testing: Design Requirements and Engineering Analysis 117
One Millinewton FEEP Thruster Tests 116
Three Body Invariant Manifold Transition with Electric Propulsion 115
Experimental Performance of Continuous and Pulsed FEEP Thrusters 114
Galileo Galilei''. Flight Experiment on the Equivalence Principle with Field Emission Electric Propulsion. GG-FEEP2, In "Small and Medium Size Italian Scientific Satellites 113
Development of a Numerical Model of the Nozzle Flow in Low Power Arcjet Thrusters 112
Experimental Investigation of a Plasma Bridge Neutralizer for a mN FEEP Thruster 111
Magneto-Plasma-Dynamic Thrusters for Space Applications 111
A 3D model for MFD flow simulation 111
Trajectory Design Considerations and Computational Tools for Electric Propulsion Missions 111
Magnetoplasmadynamic Thrusters 111
Ion Beam Modeling in FEEP Thrusters 110
Development of a LaB6 Cathode for High-Power Hall Thrusters 110
Recent Advances in Low-Current Hollow Cathodes at SITAEL 110
Kink Instabilities in a Magneto-Plasma-Dynamic Thruster With and Without External Magnetic Field 109
Fundamental Scaling Laws for Electric Propulsion Concepts - Part I: Hall Effect Thrusters 108
null 107
Further Experimental Evidences of the Development of Kink Instabilities in MPD Thrusters 107
Power Constrained Uranus Transfer and Moons Tour by Three Body Invariant Manifolds and Electric Propulsion 107
FEEP Thruster Performance at High Background Pressure 106
Filamentation Instability and Onset in MPD Thrusters 106
Experimental Study of FEEP Emitter Starting Characteristics 105
MPD Thruster Plume Diagnostics 105
FEEP Thrusters: Development Status and Prospects 105
Victor B. Tikhonov's MHD Channel Theory: A Review 105
Tunable Diode Laser Absorption for Argon Plasma Produced in an MPD Thruster 104
Experimental Investigation of Magnetohydrodynamic Instabilities in a Magneto-Plasma-Dynamic Thruster 104
Performance of an Applied Field MPD Thruster with a Pre-ionization Chamber 103
3D Model Developments for Aerospace Applications 103
Experimental Performance of a Low Power Neutralizer for a Micronewton FEEP Thruster 103
GG Drag Compensation with FEEP Thrusters 102
null 102
null 101
null 101
Hollow Cathodes for Low-Power Hall Effect Thrusters 101
Experimental Performance of Field Emission Microthrusters 100
null 100
Plasma plume diagnostics of a LaB6 hollow cathode with triple Langmuir probes 100
Spontaneous Symmetry Breaking in MPD Plasmas 99
Triple Langmuir Probes Measurements of LaB6 Hollow Cathodes Plume 99
PIC/DSMC Models for Hall Effect Thruster Plumes: Present Status and Ways Forward 98
Spontaneous Symmetry Breaking in MPD Plasmas 98
Centrospazio Progress on MPDT Hollow Cathodes 97
Electric Propulsion Activities at CENTROSPAZIO 97
High Power Plasma Thrusters in Space: European Mission Prospects 96
High Power Hall Thrusters Design Options 96
Monte Carlo Erosion Model for HT-100 Lifetime Prediction 96
Totale 11.928
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Categoria #
all - tutte 38.656
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 38.656
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20202.118 0 0 94 205 275 270 309 198 287 160 272 48
2020/20211.585 179 51 131 86 200 59 136 187 107 126 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
2024/2025328 70 237 21 0 0 0 0 0 0 0 0 0
Totale 17.755