CINECA IRIS Institutional Research Information System

MARCUCCIO, SALVO
 Distribuzione geografica
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Continente #
NA - Nord America 7.513
EU - Europa 5.684
AS - Asia 2.106
AF - Africa 267
SA - Sud America 151
OC - Oceania 128
Continente sconosciuto - Info sul continente non disponibili 3
Totale 15.852
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Nazione #
US - Stati Uniti d'America 7.212
IT - Italia 2.603
CN - Cina 710
SE - Svezia 650
DE - Germania 483
BG - Bulgaria 350
GB - Regno Unito 313
CA - Canada 278
UA - Ucraina 249
SG - Singapore 184
HK - Hong Kong 176
FR - Francia 172
TR - Turchia 164
IN - India 160
KR - Corea 140
FI - Finlandia 132
VN - Vietnam 132
AU - Australia 117
CH - Svizzera 111
ES - Italia 109
CI - Costa d'Avorio 85
BR - Brasile 79
ID - Indonesia 76
RU - Federazione Russa 74
IE - Irlanda 65
JP - Giappone 62
ZA - Sudafrica 62
NL - Olanda 60
GR - Grecia 54
IR - Iran 51
MY - Malesia 51
PL - Polonia 50
PK - Pakistan 42
PT - Portogallo 36
BE - Belgio 30
TW - Taiwan 26
AT - Austria 25
EG - Egitto 22
IL - Israele 21
MA - Marocco 21
RO - Romania 21
CZ - Repubblica Ceca 20
TN - Tunisia 20
IQ - Iraq 19
PH - Filippine 17
TH - Thailandia 16
EC - Ecuador 15
KZ - Kazakistan 15
PE - Perù 15
CL - Cile 14
CO - Colombia 14
HU - Ungheria 13
MX - Messico 12
NO - Norvegia 12
NZ - Nuova Zelanda 11
AR - Argentina 10
GH - Ghana 10
HR - Croazia 10
CR - Costa Rica 9
TZ - Tanzania 8
BY - Bielorussia 7
ET - Etiopia 7
LT - Lituania 7
SA - Arabia Saudita 7
SN - Senegal 7
KE - Kenya 6
LU - Lussemburgo 6
AE - Emirati Arabi Uniti 5
BD - Bangladesh 5
DZ - Algeria 5
OM - Oman 5
LV - Lettonia 4
MU - Mauritius 4
NG - Nigeria 4
RS - Serbia 4
SI - Slovenia 4
AZ - Azerbaigian 3
CY - Cipro 3
DK - Danimarca 3
LK - Sri Lanka 3
NP - Nepal 3
SK - Slovacchia (Repubblica Slovacca) 3
UZ - Uzbekistan 3
ZW - Zimbabwe 3
BA - Bosnia-Erzegovina 2
EU - Europa 2
JO - Giordania 2
MO - Macao, regione amministrativa speciale della Cina 2
PY - Paraguay 2
SV - El Salvador 2
A1 - Anonimo 1
BO - Bolivia 1
EE - Estonia 1
KW - Kuwait 1
LB - Libano 1
ME - Montenegro 1
MG - Madagascar 1
MN - Mongolia 1
NA - Namibia 1
SD - Sudan 1
Totale 15.851
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Città #
Woodbridge 1.132
Ann Arbor 860
Houston 742
Milan 681
Chandler 526
Seattle 386
Fairfield 369
Sofia 343
Jacksonville 324
Ottawa 245
Beijing 239
Ashburn 229
Wilmington 207
New York 202
Serra 169
Pisa 146
Princeton 144
Lawrence 133
Cambridge 119
Nanjing 119
Rome 117
Redwood City 102
Chicago 100
Singapore 100
Izmir 93
Des Moines 91
Bern 90
Dearborn 87
Abidjan 85
Livorno 80
Boardman 73
Jüchen 63
Medford 59
Florence 58
Düsseldorf 57
Hong Kong 52
London 49
Dong Ket 43
Atlanta 41
Seoul 38
Central 37
Falls Church 37
San Tung Chung Hang 36
Sydney 36
Brisbane 34
Dublin 34
Los Angeles 34
Nanchang 32
Lucca 31
Guangzhou 30
Madrid 29
Kunming 28
Shenyang 26
Frankfurt am Main 25
Padova 24
Istanbul 23
San Diego 23
Jiaxing 22
Norwalk 22
Boulder 21
Pune 21
Shanghai 21
Cascina 20
Munich 20
Bremen 19
Central District 18
Ogden 18
Tokyo 18
Brussels 17
Hebei 17
Baghdad 16
Barcelona 16
Berlin 16
Wageningen 16
Changsha 15
Hefei 15
Indiana 15
Johannesburg 15
Portoferraio 15
Bari 14
Darmstadt 14
Faisalabad 14
Helsinki 14
Massa 14
Tamworth 14
Valencia 14
Aosta 13
Gaeta 13
La Spezia 13
San Francisco 13
Santiago 13
Tehran 13
Verona 13
Washington 13
Viareggio 12
Warsaw 12
Hangzhou 11
Hyderabad 11
Jakarta 11
Kuala Lumpur 11
Totale 9.975
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Nome #
Contribution of Sentinel-2 data for applications in vegetation monitoring 2.394
EXCITE - A 12U Cubesat Mission for IOD/IOV 288
The U-PHOS experience within the ESA student REXUS/BEXUS programme: A real space hands-on opportunity 258
U-PHOS Project: Development of a Large Diameter Pulsating Heat Pipe Experiment on board REXUS 22 248
U-PHOS Project: Development of a Large Diameter Pulsating Heat Pipe Experiment on board REXUS 22 199
New Low-Cost Stratospheric Balloon Flight Opportunities with Pisa University’s MicroHAPS Platform 199
Electric Propulsion Options for Cubesats 193
U-PHOS EXPERIMENT: THERMAL RESPONSE OF A LARGE DIAMETER PULSATING HEAT PIPE ON BOARD REXUS 22 ROCKET 185
Analytical constellation design and link budget computation tool for EO missions 183
Start-up of a large diameter Pulsating Heat Pipe on ground and on board a sounding rocket 171
Analysis and Comparison of CubeSat Deorbiting Strategies 167
Flexible variable-specific-impulse electric propulsion systems for planetary missions 159
U-PHOS Project: Experimental Results of A Large Diameter Pulsating Heat Pipe on Board Rexus 22 157
L’impiego dei propulsori ad emissione di campo (FEEP) per missioni a bassissima spinta 149
A Large Space Simulator for Electric Propulsion Testing: Design Requirements and Engineering Analysis 146
Ionic Liquid Field Emission Electric Propulsion for CubeSat–Like Platforms 145
FEEP Thruster Plume Investigation with Langmuir Probes 139
null 138
A 2-D Trajectory Design Algorithm for Multiple Asteroid Flyby Missions 135
An analytical tool for quick preliminary design of remote sensing constellations with electric propulsion 133
null 132
Attitude and Orbit Control of Small Satellites and Constellations with FEEP Thrusters 128
Plasma Kinetics Issues in the ESA ‘Plasma Laboratory in Space’ Study 128
Low-Thrust Maneuvers for the Efficient Modification of Orbital Elements 127
Development of low cost solar panel with cover glass for small satellites applications 127
Galileo Galilei: Flight Experiment on the Equivalence Principle with Field Emission Electric Propulsion 125
Characterization of Linear Slit FEEP Using a Ionic Liquid Propellant 124
3-D Plume Characterization of a FEEP Thruster 124
Field Emission Electric Propulsion (FEEP) System Study 123
Experimental Behavior of FEEP Emitters Fed by a Caesium Chromate Tank 123
Electric Solar Wind Sail in tailwind 123
null 122
Control Strategies for Orbit Maintenance of LEO Small Satellites With FEEP 122
A Flight Demonstration of FEEP: Electric Thrusters for Microgravity Laboratories and Drag-Free Spacecraft 121
The Use of FEEP Systems for Micronewton Thrust Level Missions 121
Slit FEEP Thruster Performance with Ionic Liquid Propellant 120
Design and realization of a breadboard for in-space solar cells testing and characterization 119
Space-Borne Astronomical Gravity-Wave Interferometer Mission (SAGITTARIUS): The Field Emission Electric Propulsion Option 116
One Millinewton FEEP Thruster Tests 115
Integrated Trajectory and Energy Management Simulator for Electric Propulsion Spacecraft 114
Flight Campaign Results and Prospects of High-Altitude Balloons for Low Cost Spacecraft Technology Testing 114
Experimental Performance of Continuous and Pulsed FEEP Thrusters 113
Experimental Investigation of the Simultaneous Firing of Two FEEP Thrusters 113
Galileo Galilei''. Flight Experiment on the Equivalence Principle with Field Emission Electric Propulsion. GG-FEEP2, In "Small and Medium Size Italian Scientific Satellites 112
Experimental Investigation of a Plasma Bridge Neutralizer for a mN FEEP Thruster 110
AFM Characterization of the FEEP Microthruster 110
Smaller Satellites, Larger Constellations: Trends and Design Issues for Earth Observation Systems 110
Ion Beam Modeling in FEEP Thrusters 109
Low-thrust Transfers for the Vega Electric Upper Stage 109
Ionic Liquid FEEP: Recent Experimental Results 109
Endurance Test of the Micronewton FEEP Thruster 108
null 107
Fundamental Scaling Laws for Electric Propulsion Concepts - Part I: Hall Effect Thrusters 107
FEEP Thruster Performance at High Background Pressure 105
Development and Test of Low Cost Solar Panel Technologies for Small Satellites 104
FEEP Thrusters: Development Status and Prospects 103
Experimental Study of FEEP Emitter Starting Characteristics 102
Experimental Performance of a Low Power Neutralizer for a Micronewton FEEP Thruster 102
GG Drag Compensation with FEEP Thrusters 101
The New European Propulsion Standard 101
null 101
The ECAPS Experiment for Solar Cell Characterization in the Stratosphere 101
null 100
Experimental Performance of Field Emission Microthrusters 98
Upgraded Pulsating Heat Pipe Only For Space (U-Phos): Results of the 22nd Rexus Sounding Rocket Campaign 98
FEEP New Propellants CCN2 - Final Report 96
Electric Propulsion Activities at CENTROSPAZIO 96
Combination of Landsat 8 and Sentinel 1 data for the characterization of a site of interest. A Case Study: the Royal Palace of Caserta 96
IL-FEEP: a Simplified, Low Cost Electric Thruster for Micro- and Nano-Satellites 95
European Perspective on Research Problems in Micro-Electric Devices 94
Development of a Miniaturized Electric Propulsion System for the E-Sail Project 94
A 2-D Trajectory Design Algorithm for Multiple Asteroid Flyby Missions 93
Drag-Free, Attitude and Orbit Control for LISA 92
Surveillance Constellations of Low Altitude Small Satellites with Electric Propulsion 92
E-Plus: Extending the Operational Envelope of Small Launchers with an Auxiliary Electric Platform 91
FEEP System for the Microscope Mission 89
FEEP Microthruster Technology Status and Potential Applications 88
Design of a Manoeuvrable CubeSat Deployment Vehicle Equipped with Electric Propulsion 87
Tecnologie per i piccoli satelliti: realizzazioni e prospettive presso l’Università di Pisa 87
Catodi ad ossidi di terre alcaline per impieghi spaziali 84
Challenges and Solutions for the QB50 Telecommunication Network 84
Validation Flight Experiment for a Sounding Balloon Photovoltaic-based Attitude Determination System 83
Plasma kinetics issues in an ESA study for a plasma laboratory in space 82
null 82
Low Power HET Flight Demonstration and Plasma Experiments on a Microsatellite 81
High Power Electric Propulsion for a Flexible Space Exploration Architecture 81
A High-Power Electric Propulsion Test Facility 79
Low Cost Solar Panel for Microsatellites 79
Earth Observation from Elliptical Orbits with Very Low Altitude Perigee 78
FEEP Micropropulsion Systems for Scientific Missions 78
Active Plasma Experiments in Space: a Small Satellite Mission 78
Status and Perspectives of Electric Propulsion in Italy 77
null 77
Dynamic Characterization of a High-Altitude Balloon During a Flight Campaign for the Detection of ISM Radio Background in the Stratosphere 77
Ceres Lander Exploration and Sample Return Mission 76
Innovative Field Emission Microthrusters for Scientific Missions 76
Preliminary Assessment of a Solar Wind Shield Based on a Plasma-Inflated Artificial Magnetosphere 74
Joint Trajectory and Energy Management Simulation of Low Thrust Missions 74
Flexible variable-specific-impulse electric propulsion systems for planetary missions 74
E-Plus: Electric Propulsion Equipped Launchers Upper Stage 73
Totale 13.824
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Categoria #
all - tutte 32.656
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 32.656
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20201.637 0 183 96 136 172 197 181 103 163 159 188 59
2020/20211.435 108 66 97 62 150 116 137 131 146 136 92 194
2021/20222.036 48 188 59 128 352 275 81 95 143 56 199 412
2022/20232.145 295 209 124 199 263 320 93 125 324 56 97 40
2023/20243.538 320 286 318 276 387 410 362 174 96 237 325 347
2024/2025209 163 46 0 0 0 0 0 0 0 0 0 0
Totale 16.170