CINECA IRIS Institutional Research Information System

MARCUCCIO, SALVO
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 11.160
EU - Europa 8.281
AS - Asia 7.294
SA - Sud America 863
AF - Africa 424
Continente sconosciuto - Info sul continente non disponibili 371
OC - Oceania 214
Totale 28.607
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 10.678
IT - Italia 3.726
CN - Cina 1.887
SG - Singapore 1.737
HK - Hong Kong 1.156
DE - Germania 699
SE - Svezia 694
BR - Brasile 667
GB - Regno Unito 519
KR - Corea 448
VN - Vietnam 448
FR - Francia 389
CA - Canada 357
BG - Bulgaria 355
IN - India 324
UA - Ucraina 296
TR - Turchia 270
RU - Federazione Russa 238
JP - Giappone 218
FI - Finlandia 213
ES - Italia 208
AU - Australia 189
CH - Svizzera 184
ID - Indonesia 161
NL - Olanda 149
ZA - Sudafrica 133
IE - Irlanda 102
PL - Polonia 89
CI - Costa d'Avorio 85
IR - Iran 75
PH - Filippine 68
AT - Austria 66
MY - Malesia 65
TW - Taiwan 65
GR - Grecia 60
PK - Pakistan 58
IQ - Iraq 53
PT - Portogallo 51
AR - Argentina 45
MX - Messico 44
BD - Bangladesh 41
EG - Egitto 38
BE - Belgio 37
CR - Costa Rica 36
IL - Israele 36
TN - Tunisia 35
CZ - Repubblica Ceca 34
EC - Ecuador 33
PE - Perù 31
CO - Colombia 30
MA - Marocco 30
CL - Cile 28
RO - Romania 25
KZ - Kazakistan 23
SA - Arabia Saudita 23
TH - Thailandia 22
UZ - Uzbekistan 20
HU - Ungheria 19
KE - Kenya 17
AE - Emirati Arabi Uniti 15
DZ - Algeria 15
LT - Lituania 15
NZ - Nuova Zelanda 15
DK - Danimarca 14
HR - Croazia 14
NO - Norvegia 14
LU - Lussemburgo 12
LK - Sri Lanka 11
SN - Senegal 11
BY - Bielorussia 10
EE - Estonia 10
ET - Etiopia 10
GH - Ghana 10
JM - Giamaica 10
TZ - Tanzania 10
VE - Venezuela 10
LB - Libano 9
AZ - Azerbaigian 8
OM - Oman 8
PY - Paraguay 8
RS - Serbia 8
SK - Slovacchia (Repubblica Slovacca) 8
LV - Lettonia 7
NP - Nepal 7
SV - El Salvador 7
GT - Guatemala 6
SI - Slovenia 6
TT - Trinidad e Tobago 6
CY - Cipro 5
JO - Giordania 5
MG - Madagascar 5
MU - Mauritius 5
NC - Nuova Caledonia 5
NG - Nigeria 5
UY - Uruguay 5
BA - Bosnia-Erzegovina 4
BO - Bolivia 4
KW - Kuwait 4
ZW - Zimbabwe 4
CG - Congo 3
Totale 28.175
Salva come PNG Salva come JPEG
Città #
Woodbridge 1.133
Singapore 1.058
Hong Kong 985
Ashburn 918
Ann Arbor 860
Milan 751
Houston 747
San Jose 645
Santa Clara 575
Chandler 527
Seattle 396
Pisa 390
Fairfield 370
Beijing 348
Sofia 347
Hefei 329
Jacksonville 326
Seoul 284
Dallas 277
Shanghai 271
Ottawa 247
New York 236
Boardman 218
Wilmington 207
Rome 191
Serra 169
Los Angeles 159
Princeton 145
Lawrence 133
Lauterbourg 128
Tokyo 127
Ho Chi Minh City 123
Nanjing 121
Cambridge 119
Chicago 113
Florence 111
Council Bluffs 103
Livorno 102
Redwood City 102
Munich 98
Istanbul 94
Izmir 94
Des Moines 93
Bern 92
Hanoi 90
Dearborn 87
Abidjan 85
Helsinki 67
Düsseldorf 66
Buffalo 63
Jüchen 63
Zurich 63
Atlanta 59
Frankfurt am Main 59
London 59
Medford 59
Dublin 57
Sydney 57
Lucca 56
Redondo Beach 52
Brisbane 50
Dong Ket 43
Bologna 40
Madrid 38
Central 37
Falls Church 37
São Paulo 37
Barcelona 36
Guangzhou 36
San Tung Chung Hang 36
Nanchang 34
Dnipro 33
Fuzhou 32
Jakarta 32
Johannesburg 30
Naples 30
Pune 30
Turin 30
Warsaw 30
Baghdad 29
Kunming 29
Manchester 29
Cascina 28
Chennai 28
Vienna 28
Durban 27
Orem 27
Shenyang 27
Berlin 26
Dresden 26
Amsterdam 25
Padova 25
San Diego 25
Taipei 25
Paris 24
Bengaluru 23
Boulder 23
Brasília 23
San Francisco 23
Washington 23
Totale 17.118
Salva come PNG Salva come JPEG
Nome #
Contribution of Sentinel-2 data for applications in vegetation monitoring 3.511
EXCITE - A 12U Cubesat Mission for IOD/IOV 560
The U-PHOS experience within the ESA student REXUS/BEXUS programme: A real space hands-on opportunity 397
U-PHOS Project: Development of a Large Diameter Pulsating Heat Pipe Experiment on board REXUS 22 365
New Low-Cost Stratospheric Balloon Flight Opportunities with Pisa University’s MicroHAPS Platform 355
Development of the EXCITE IOD/IOV mission 334
U-PHOS Project: Development of a Large Diameter Pulsating Heat Pipe Experiment on board REXUS 22 326
Analytical constellation design and link budget computation tool for EO missions 317
U-PHOS Project: Experimental Results of A Large Diameter Pulsating Heat Pipe on Board Rexus 22 294
U-PHOS EXPERIMENT: THERMAL RESPONSE OF A LARGE DIAMETER PULSATING HEAT PIPE ON BOARD REXUS 22 ROCKET 286
ARAMMIS: Autonomous Robots for Area Mapping, Monitoring and In-situ gas Sensing, focused on Lunar exploration and Earth Science applications 275
Start-up of a large diameter Pulsating Heat Pipe on ground and on board a sounding rocket 272
Electric Propulsion Options for Cubesats 258
Analysis and Comparison of CubeSat Deorbiting Strategies 244
L’impiego dei propulsori ad emissione di campo (FEEP) per missioni a bassissima spinta 238
Low-Thrust Maneuvers for the Efficient Modification of Orbital Elements 222
Analysis of the Feasibility of a Low-Cost DAQ for EM-38 Detection and Mapping 216
Ionic Liquid Field Emission Electric Propulsion for CubeSat–Like Platforms 214
Flight Campaign Results and Prospects of High-Altitude Balloons for Low Cost Spacecraft Technology Testing 212
Flexible variable-specific-impulse electric propulsion systems for planetary missions 210
The ECAPS Experiment for Solar Cell Characterization in the Stratosphere 210
FEEP Thruster Plume Investigation with Langmuir Probes 207
Ceres Lander Exploration and Sample Return Mission 205
Prospects of the µHAPS Miniaturised Stratospheric Platform for Remote Sensing and Environmental Monitoring in Light of Recent Flight Demonstrations 204
Dynamic Characterization of a High-Altitude Balloon During a Flight Campaign for the Detection of ISM Radio Background in the Stratosphere 201
A 2-D Trajectory Design Algorithm for Multiple Asteroid Flyby Missions 194
Experimental Study of FEEP Emitter Starting Characteristics 193
Electric Solar Wind Sail in tailwind 193
An analytical tool for quick preliminary design of remote sensing constellations with electric propulsion 193
Galileo Galilei: Flight Experiment on the Equivalence Principle with Field Emission Electric Propulsion 190
A Flight Demonstration of FEEP: Electric Thrusters for Microgravity Laboratories and Drag-Free Spacecraft 189
Space-Borne Astronomical Gravity-Wave Interferometer Mission (SAGITTARIUS): The Field Emission Electric Propulsion Option 188
Experimental Behavior of FEEP Emitters Fed by a Caesium Chromate Tank 187
Attitude and Orbit Control of Small Satellites and Constellations with FEEP Thrusters 187
Experimental Investigation of a Plasma Bridge Neutralizer for a mN FEEP Thruster 186
Plasma Kinetics Issues in the ESA ‘Plasma Laboratory in Space’ Study 185
Development of low cost solar panel with cover glass for small satellites applications 185
Characterization of Linear Slit FEEP Using a Ionic Liquid Propellant 184
A Large Space Simulator for Electric Propulsion Testing: Design Requirements and Engineering Analysis 184
Field Emission Electric Propulsion (FEEP) System Study 183
Smaller Satellites, Larger Constellations: Trends and Design Issues for Earth Observation Systems 183
Ion Beam Modeling in FEEP Thrusters 180
Integrated Trajectory and Energy Management Simulator for Electric Propulsion Spacecraft 178
IL-FEEP: a Simplified, Low Cost Electric Thruster for Micro- and Nano-Satellites 177
Experimental Performance of Continuous and Pulsed FEEP Thrusters 176
One Millinewton FEEP Thruster Tests 175
Development and Test of Low Cost Solar Panel Technologies for Small Satellites 175
The Use of FEEP Systems for Micronewton Thrust Level Missions 174
A multi-gas sensor system lifted by a tethered aerostat for real time in-situ investigation of volcanic plumes 173
Validation Flight Experiment for a Sounding Balloon Photovoltaic-based Attitude Determination System 173
FEEP Thruster Performance at High Background Pressure 172
Galileo Galilei''. Flight Experiment on the Equivalence Principle with Field Emission Electric Propulsion. GG-FEEP2, In "Small and Medium Size Italian Scientific Satellites 171
FEEP Thrusters: Development Status and Prospects 171
Design and realization of a breadboard for in-space solar cells testing and characterization 169
Control Strategies for Orbit Maintenance of LEO Small Satellites With FEEP 169
Direct measurements in volcanic plumes using balloon-borne multi-gas and particles sensor systems. The Vulcano Island and Etna 2025 field campaigns 166
AFM Characterization of the FEEP Microthruster 166
Slit FEEP Thruster Performance with Ionic Liquid Propellant 166
GG Drag Compensation with FEEP Thrusters 165
Experimental Investigation of the Simultaneous Firing of Two FEEP Thrusters 164
Upgraded Pulsating Heat Pipe Only For Space (U-Phos): Results of the 22nd Rexus Sounding Rocket Campaign 164
Fundamental Scaling Laws for Electric Propulsion Concepts - Part I: Hall Effect Thrusters 162
FEEP Micropropulsion Systems for Scientific Missions 162
Combination of Landsat 8 and Sentinel 1 data for the characterization of a site of interest. A Case Study: the Royal Palace of Caserta 160
Experimental Performance of a Low Power Neutralizer for a Micronewton FEEP Thruster 159
Drag-Free, Attitude and Orbit Control for LISA 158
Ionic Liquid FEEP: Recent Experimental Results 157
3-D Plume Characterization of a FEEP Thruster 155
Low-thrust Transfers for the Vega Electric Upper Stage 154
Endurance Test of the Micronewton FEEP Thruster 154
The New European Propulsion Standard 153
Experimental Performance of Field Emission Microthrusters 152
FEEP Microthruster Technology Status and Potential Applications 148
Science, Technology and Systems Engineering Educational Activities with Stratospheric Balloons 148
FEEP Thruster Survivability in the LEO Atomic Oxygen Environment 147
A 2-D Trajectory Design Algorithm for Multiple Asteroid Flyby Missions 147
Navigation of Sounding Balloons with Deep Reinforcement Learning 146
European Perspective on Research Problems in Micro-Electric Devices 146
FEEP New Propellants CCN2 - Final Report 146
FEEP System for the Microscope Mission 145
Surveillance Constellations of Low Altitude Small Satellites with Electric Propulsion 143
A Custom Radiosonde Design for Environmental Measurements Over Maritime Areas 141
Development of a Miniaturized Electric Propulsion System for the E-Sail Project 140
null 140
null 138
Preliminary Assessment of a Solar Wind Shield Based on a Plasma-Inflated Artificial Magnetosphere 137
Challenges and Solutions for the QB50 Telecommunication Network 137
E-Plus: Extending the Operational Envelope of Small Launchers with an Auxiliary Electric Platform 136
FEEP Thrusters Applications to Constellations and Small Satellites 135
Electric Propulsion Activities at CENTROSPAZIO 134
Design of a Manoeuvrable CubeSat Deployment Vehicle Equipped with Electric Propulsion 134
Plasma kinetics issues in an ESA study for a plasma laboratory in space 133
null 132
Tecnologie per i piccoli satelliti: realizzazioni e prospettive presso l’Università di Pisa 132
Active Plasma Experiments in Space: a Small Satellite Mission 131
Low-Thrust Propulsion Systems for Small Satellites 129
Joint Trajectory and Energy Management Simulation of Low Thrust Missions 128
Low Cost Solar Panel for Microsatellites 127
Earth Observation from Elliptical Orbits with Very Low Altitude Perigee 126
Low Power HET Flight Demonstration and Plasma Experiments on a Microsatellite 126
Totale 22.139
Salva come PNG Salva come JPEG
Categoria #
all - tutte 66.140
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 66.140
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20221.988 0 188 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
2024/20255.554 163 302 165 393 514 523 354 349 592 678 667 854
2025/20266.718 343 805 576 704 690 545 889 368 473 720 249 356
2026/2027374 302 72 0 0 0 0 0 0 0 0 0 0
Totale 28.607