CINECA IRIS Institutional Research Information System

MARCUCCIO, SALVO
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 10.956
EU - Europa 8.067
AS - Asia 7.269
SA - Sud America 853
AF - Africa 422
OC - Oceania 213
Continente sconosciuto - Info sul continente non disponibili 3
Totale 27.783
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 10.494
IT - Italia 3.563
CN - Cina 1.881
SG - Singapore 1.736
HK - Hong Kong 1.152
DE - Germania 689
SE - Svezia 669
BR - Brasile 662
GB - Regno Unito 516
VN - Vietnam 446
KR - Corea 445
FR - Francia 389
BG - Bulgaria 355
CA - Canada 350
IN - India 323
UA - Ucraina 294
TR - Turchia 270
RU - Federazione Russa 238
JP - Giappone 216
FI - Finlandia 213
ES - Italia 207
AU - Australia 189
CH - Svizzera 180
ID - Indonesia 158
NL - Olanda 146
ZA - Sudafrica 131
IE - Irlanda 102
PL - Polonia 88
CI - Costa d'Avorio 85
IR - Iran 75
PH - Filippine 67
AT - Austria 66
MY - Malesia 65
TW - Taiwan 65
GR - Grecia 60
PK - Pakistan 58
IQ - Iraq 53
PT - Portogallo 51
AR - Argentina 44
BD - Bangladesh 41
MX - Messico 41
EG - Egitto 38
BE - Belgio 37
IL - Israele 36
CR - Costa Rica 35
TN - Tunisia 35
CZ - Repubblica Ceca 34
EC - Ecuador 31
PE - Perù 31
MA - Marocco 30
CO - Colombia 29
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
DK - Danimarca 14
HR - Croazia 14
NO - Norvegia 14
NZ - Nuova Zelanda 14
LK - Sri Lanka 11
LU - Lussemburgo 11
SN - Senegal 11
BY - Bielorussia 10
EE - Estonia 10
ET - Etiopia 10
GH - Ghana 10
TZ - Tanzania 10
VE - Venezuela 10
LB - Libano 9
AZ - Azerbaigian 8
JM - Giamaica 8
OM - Oman 8
PY - Paraguay 8
RS - Serbia 8
SK - Slovacchia (Repubblica Slovacca) 8
LV - Lettonia 7
NP - Nepal 7
SI - Slovenia 6
SV - El Salvador 6
TT - Trinidad e Tobago 6
CY - Cipro 5
GT - Guatemala 5
JO - Giordania 5
MG - Madagascar 5
MU - Mauritius 5
NC - Nuova Caledonia 5
NG - Nigeria 5
BO - Bolivia 4
KW - Kuwait 4
UY - Uruguay 4
ZW - Zimbabwe 4
BA - Bosnia-Erzegovina 3
CG - Congo 3
Totale 27.726
Salva come PNG Salva come JPEG
Città #
Woodbridge 1.133
Singapore 1.057
Hong Kong 982
Ashburn 896
Ann Arbor 860
Houston 747
Milan 744
San Jose 639
Santa Clara 566
Chandler 527
Seattle 395
Fairfield 370
Sofia 347
Beijing 343
Hefei 329
Jacksonville 325
Pisa 312
Seoul 282
Dallas 275
Shanghai 271
Ottawa 247
New York 232
Boardman 218
Wilmington 207
Rome 186
Serra 169
Los Angeles 156
Princeton 145
Lawrence 133
Lauterbourg 128
Tokyo 127
Ho Chi Minh City 122
Nanjing 121
Cambridge 119
Chicago 110
Florence 107
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
Jüchen 63
Buffalo 62
Zurich 62
London 59
Medford 59
Atlanta 57
Dublin 57
Frankfurt am Main 57
Sydney 57
Council Bluffs 56
Lucca 55
Redondo Beach 52
Brisbane 50
Dong Ket 43
Madrid 38
Central 37
Falls Church 37
São Paulo 37
Barcelona 36
Bologna 36
Guangzhou 36
San Tung Chung Hang 36
Nanchang 34
Dnipro 33
Fuzhou 32
Jakarta 32
Johannesburg 30
Pune 30
Turin 30
Warsaw 30
Baghdad 29
Kunming 29
Manchester 29
Cascina 28
Chennai 28
Naples 28
Vienna 28
Orem 27
Shenyang 27
Berlin 26
Amsterdam 25
Durban 25
Padova 25
San Diego 25
Taipei 25
Paris 24
Boulder 23
Brasília 23
Bengaluru 22
Changsha 22
Jiaxing 22
Norwalk 22
Totale 16.892
Salva come PNG Salva come JPEG
Nome #
Contribution of Sentinel-2 data for applications in vegetation monitoring 3.492
EXCITE - A 12U Cubesat Mission for IOD/IOV 549
The U-PHOS experience within the ESA student REXUS/BEXUS programme: A real space hands-on opportunity 392
U-PHOS Project: Development of a Large Diameter Pulsating Heat Pipe Experiment on board REXUS 22 360
New Low-Cost Stratospheric Balloon Flight Opportunities with Pisa University’s MicroHAPS Platform 351
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 307
Development of the EXCITE IOD/IOV mission 295
U-PHOS Project: Experimental Results of A Large Diameter Pulsating Heat Pipe on Board Rexus 22 293
U-PHOS EXPERIMENT: THERMAL RESPONSE OF A LARGE DIAMETER PULSATING HEAT PIPE ON BOARD REXUS 22 ROCKET 286
Start-up of a large diameter Pulsating Heat Pipe on ground and on board a sounding rocket 271
Electric Propulsion Options for Cubesats 257
ARAMMIS: Autonomous Robots for Area Mapping, Monitoring and In-situ gas Sensing, focused on Lunar exploration and Earth Science applications 255
Analysis and Comparison of CubeSat Deorbiting Strategies 243
L’impiego dei propulsori ad emissione di campo (FEEP) per missioni a bassissima spinta 237
Low-Thrust Maneuvers for the Efficient Modification of Orbital Elements 220
Analysis of the Feasibility of a Low-Cost DAQ for EM-38 Detection and Mapping 211
Ionic Liquid Field Emission Electric Propulsion for CubeSat–Like Platforms 211
Flexible variable-specific-impulse electric propulsion systems for planetary missions 210
The ECAPS Experiment for Solar Cell Characterization in the Stratosphere 207
FEEP Thruster Plume Investigation with Langmuir Probes 203
Flight Campaign Results and Prospects of High-Altitude Balloons for Low Cost Spacecraft Technology Testing 202
Ceres Lander Exploration and Sample Return Mission 198
Dynamic Characterization of a High-Altitude Balloon During a Flight Campaign for the Detection of ISM Radio Background in the Stratosphere 197
A 2-D Trajectory Design Algorithm for Multiple Asteroid Flyby Missions 193
An analytical tool for quick preliminary design of remote sensing constellations with electric propulsion 192
Prospects of the µHAPS Miniaturised Stratospheric Platform for Remote Sensing and Environmental Monitoring in Light of Recent Flight Demonstrations 191
Experimental Study of FEEP Emitter Starting Characteristics 190
Electric Solar Wind Sail in tailwind 190
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 188
Attitude and Orbit Control of Small Satellites and Constellations with FEEP Thrusters 187
Space-Borne Astronomical Gravity-Wave Interferometer Mission (SAGITTARIUS): The Field Emission Electric Propulsion Option 186
Experimental Behavior of FEEP Emitters Fed by a Caesium Chromate Tank 185
Plasma Kinetics Issues in the ESA ‘Plasma Laboratory in Space’ Study 185
A Large Space Simulator for Electric Propulsion Testing: Design Requirements and Engineering Analysis 184
Field Emission Electric Propulsion (FEEP) System Study 183
Experimental Investigation of a Plasma Bridge Neutralizer for a mN FEEP Thruster 183
Smaller Satellites, Larger Constellations: Trends and Design Issues for Earth Observation Systems 183
Development of low cost solar panel with cover glass for small satellites applications 182
Ion Beam Modeling in FEEP Thrusters 178
Integrated Trajectory and Energy Management Simulator for Electric Propulsion Spacecraft 178
Characterization of Linear Slit FEEP Using a Ionic Liquid Propellant 177
Experimental Performance of Continuous and Pulsed FEEP Thrusters 175
IL-FEEP: a Simplified, Low Cost Electric Thruster for Micro- and Nano-Satellites 175
The Use of FEEP Systems for Micronewton Thrust Level Missions 174
One Millinewton FEEP Thruster Tests 174
Development and Test of Low Cost Solar Panel Technologies for Small Satellites 173
Validation Flight Experiment for a Sounding Balloon Photovoltaic-based Attitude Determination System 173
FEEP Thruster Performance at High Background Pressure 171
FEEP Thrusters: Development Status and Prospects 170
Galileo Galilei''. Flight Experiment on the Equivalence Principle with Field Emission Electric Propulsion. GG-FEEP2, In "Small and Medium Size Italian Scientific Satellites 169
Control Strategies for Orbit Maintenance of LEO Small Satellites With FEEP 169
A multi-gas sensor system lifted by a tethered aerostat for real time in-situ investigation of volcanic plumes 168
Design and realization of a breadboard for in-space solar cells testing and characterization 168
AFM Characterization of the FEEP Microthruster 166
GG Drag Compensation with FEEP Thrusters 165
Experimental Investigation of the Simultaneous Firing of Two FEEP Thrusters 164
Slit FEEP Thruster Performance with Ionic Liquid Propellant 164
Fundamental Scaling Laws for Electric Propulsion Concepts - Part I: Hall Effect Thrusters 161
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
Upgraded Pulsating Heat Pipe Only For Space (U-Phos): Results of the 22nd Rexus Sounding Rocket Campaign 160
FEEP Micropropulsion Systems for Scientific Missions 159
Drag-Free, Attitude and Orbit Control for LISA 158
Experimental Performance of a Low Power Neutralizer for a Micronewton FEEP Thruster 158
Ionic Liquid FEEP: Recent Experimental Results 156
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
Experimental Performance of Field Emission Microthrusters 151
The New European Propulsion Standard 150
Direct measurements in volcanic plumes using balloon-borne multi-gas and particles sensor systems. The Vulcano Island and Etna 2025 field campaigns 147
Science, Technology and Systems Engineering Educational Activities with Stratospheric Balloons 147
FEEP Microthruster Technology Status and Potential Applications 146
European Perspective on Research Problems in Micro-Electric Devices 146
FEEP New Propellants CCN2 - Final Report 146
A 2-D Trajectory Design Algorithm for Multiple Asteroid Flyby Missions 145
FEEP System for the Microscope Mission 144
FEEP Thruster Survivability in the LEO Atomic Oxygen Environment 144
Surveillance Constellations of Low Altitude Small Satellites with Electric Propulsion 142
Navigation of Sounding Balloons with Deep Reinforcement Learning 140
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
A Custom Radiosonde Design for Environmental Measurements Over Maritime Areas 136
E-Plus: Extending the Operational Envelope of Small Launchers with an Auxiliary Electric Platform 135
Plasma kinetics issues in an ESA study for a plasma laboratory in space 133
Electric Propulsion Activities at CENTROSPAZIO 133
null 132
FEEP Thrusters Applications to Constellations and Small Satellites 132
Design of a Manoeuvrable CubeSat Deployment Vehicle Equipped with Electric Propulsion 132
Tecnologie per i piccoli satelliti: realizzazioni e prospettive presso l’Università di Pisa 132
Active Plasma Experiments in Space: a Small Satellite Mission 130
Joint Trajectory and Energy Management Simulation of Low Thrust Missions 127
Low-Thrust Propulsion Systems for Small Satellites 127
Earth Observation from Elliptical Orbits with Very Low Altitude Perigee 126
Low Power HET Flight Demonstration and Plasma Experiments on a Microsatellite 126
Evolution of the (Aero)Space Engineering Studies in Italy in the past 20 years 126
Totale 21.858
Salva come PNG Salva come JPEG
Categoria #
all - tutte 63.743
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 63.743
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021194 0 0 0 0 0 0 0 0 0 0 0 194
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
2024/20255.554 163 302 165 393 514 523 354 349 592 678 667 854
2025/20266.636 343 805 576 704 690 545 889 368 473 720 249 274
Totale 28.151