OLIVIERI, LORENZO
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 3.963
EU - Europa 2.881
AS - Asia 1.936
SA - Sud America 45
OC - Oceania 23
AF - Africa 19
Continente sconosciuto - Info sul continente non disponibili 1
Totale 8.868
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 3.916
IT - Italia 1.653
CN - Cina 682
SG - Singapore 642
DE - Germania 257
JP - Giappone 207
FI - Finlandia 162
FR - Francia 139
GB - Regno Unito 130
IN - India 129
ES - Italia 119
RU - Federazione Russa 92
HK - Hong Kong 87
NL - Olanda 87
KR - Corea 55
SE - Svezia 51
CA - Canada 40
PL - Polonia 29
IR - Iran 21
UA - Ucraina 21
BE - Belgio 20
IE - Irlanda 20
VN - Vietnam 18
CH - Svizzera 16
TW - Taiwan 16
AU - Australia 15
ID - Indonesia 14
BR - Brasile 13
AT - Austria 11
NO - Norvegia 11
PE - Perù 11
TR - Turchia 11
CL - Cile 10
PH - Filippine 10
EG - Egitto 9
MT - Malta 9
PT - Portogallo 9
CZ - Repubblica Ceca 8
LU - Lussemburgo 8
NZ - Nuova Zelanda 8
MY - Malesia 7
SA - Arabia Saudita 6
CO - Colombia 5
HU - Ungheria 5
MA - Marocco 5
RO - Romania 5
TH - Thailandia 5
AE - Emirati Arabi Uniti 4
BG - Bulgaria 4
IQ - Iraq 4
BD - Bangladesh 3
BO - Bolivia 3
GR - Grecia 3
IL - Israele 3
LT - Lituania 3
MO - Macao, regione amministrativa speciale della Cina 3
MX - Messico 3
OM - Oman 3
AR - Argentina 2
EE - Estonia 2
KE - Kenya 2
RS - Serbia 2
SI - Slovenia 2
BA - Bosnia-Erzegovina 1
CR - Costa Rica 1
CY - Cipro 1
DK - Danimarca 1
DO - Repubblica Dominicana 1
DZ - Algeria 1
EC - Ecuador 1
ET - Etiopia 1
EU - Europa 1
GT - Guatemala 1
JO - Giordania 1
KG - Kirghizistan 1
KZ - Kazakistan 1
LV - Lettonia 1
NG - Nigeria 1
NP - Nepal 1
PA - Panama 1
TM - Turkmenistan 1
Totale 8.868
Salva come PNG Salva come JPEG
Città #
Singapore 469
Chandler 460
Padova 390
Beijing 316
Fairfield 310
Ashburn 286
Boardman 272
Houston 242
Santa Clara 229
Ann Arbor 212
Woodbridge 199
Cambridge 164
Milan 133
Seattle 120
Helsinki 113
Osaka 107
Wilmington 101
Medford 85
Princeton 85
Des Moines 72
Verona 69
Madrid 67
Munich 64
Rome 56
San Diego 53
Hong Kong 49
Venice 36
Tokyo 35
Jacksonville 30
Dallas 27
Reggio Emilia 24
Getafe 23
Nanjing 23
Shanghai 23
Lavis 21
Los Angeles 21
Paese 21
Treviso 21
Guangzhou 20
New York 19
Turin 19
Dublin 18
Falkenstein 17
Vicenza 17
Trieste 16
Bengaluru 15
Dong Ket 15
Lappeenranta 15
Washington 15
Newton 14
Ogden 14
Council Bluffs 13
Fossò 13
Frankfurt am Main 13
Paris 13
Pune 13
Glasgow 12
Kochi 12
London 12
Martellago 12
Shenyang 12
Toronto 12
Amsterdam 11
Brendola 11
Jinan 11
Budrio 10
Columbus 10
Hebei 10
Hyderabad 10
Lima 10
Mumbai 10
Florence 9
Harbin 9
Hengyang 9
Nottingham 9
Taipei 9
Zurich 9
Braunschweig 8
Brussels 8
Chicago 8
Dresden 8
Jiaxing 8
Leeds 8
Leicester 8
Melbourne 8
Naples 8
Nuremberg 8
Ottawa 8
Roxbury 8
Seoul 8
Shinkōchō 8
Southampton 8
Berlin 7
Cagliari 7
Edmonton 7
Follonica 7
Gallarate 7
Kyoto 7
Nagoya 7
Pescara 7
Totale 5.702
Salva come PNG Salva come JPEG
Nome #
DESIGN OF DOCKING MECHANISM FOR SMALL SPACECRAFT 346
Fragments Distribution Prediction for ENVISAT Catastrophic Fragmentation 340
Deorbiting Perfomance of Electrodynamic Tethers to Mitigate Space Debris 190
Development and characterization of a standardized docking system for small spacecraft 172
Design and testing of an autonomous ARTVA detector for small drones 156
ARCADE‑R2 EXPERIMENT ON BOARD BEXUS 17 STRATOSPHERIC BALLOON 145
Development of a low-cost sun sensor for nanosatellites 145
Space tethers: parameters reconstructions and tests 145
CST: A new semi-empirical tool for simulating spacecraft collisions in orbit 135
An innovative space tether deployer with retrieval capability: design and test of star experiment 135
Cubesat mission concept for tethered electromagnetic docking demonstration 133
EXPERIMENTAL VALIDATION OF A DEPLOYMENT MECHANISM FOR TAPE-TETHERED SATELLITES 129
Deorbit kit demonstration mission 128
AlbaSat: an educational satellite for a multi-objective mission in LEO 122
CST: a new semi-empirical tool for simulating spacecraft collisions in orbit 120
TED project: Conjugating technology development and educational activities 116
ERMES: Experimental Rendezvous in Microgravity Environment Study 115
e.Cube Mission: the Environmental CubeSat 114
A STUDENT EXPERIMENT FROM STRATOSPHERIC BALLOON BEXUS 10: SCRAT FROM CONCEPT TO LAUNCH 113
Advances in the characterisation of collision break-ups by means of numerical modelling 97
Test of Tethered Deorbiting of Space Debris 94
Study of dynamical stability of tethered systems during space tug maneuvers 91
ALBASAT: AN EDUCATIONAL SATELLITE FOR A MULTI-OBJECTIVES MISSION IN LEO 90
Miniature docking mechanism for CubeSats 89
Development Roadmap of a Deorbit Kit Based on Electrodynamic Tether Technology 89
Deployment requirements for deorbiting electrodynamic tether technology 88
Autoport project: A docking station for planetary exploration drones 84
A CubeSat-sized space debris impact sensor 84
Autonomous Rendezvous, Control and Docking Experiment – Reflight 2 83
A new concept variable resistance radiator 83
A new concept of variable resistance radiator: Stratospheric flight test and performance analysis 81
Laser Vibrometry Based Precise Measurement of Tape-Shaped Tethers Damping Ratio Towards Space Applications 79
Retrieval Strategies for Tethered Satellites 77
Semi-androgynous multifunctional interface for expandable space structures 76
An analitycal method for the propagation towards internal components of debris clouds originated by space debris impacts on spacecraft walls 75
An in-line damper for tethers-in-space oscillations dissipation 75
Overview of the AlbaSat mission the first CubeSat from University of Padova 74
Arcade experiment on board bexus 13 and 17: Design, integration and flight of a technology test platform within a student balloon programme 74
Data retrieved by SCRAT experiment during the 2010 ESA BEXUS 10 flight campaign 73
Examination of satellite collision scenarios spanning low to hypervelocity encounters using semi-empirical models 73
AVERLA: autonomous drone for avalanche rescue 72
Flexible electromagnetic leash docking system (felds) experiment from design to microgravity testing 72
Low-cost relative navigation sensors for miniature spacecraft and drones 71
The ATEMO device: a compact solution for earth monitoring 71
Design and test of a semiandrogynous docking mechanism for small satellites 70
Avalanche Rescue with Autonomous Drones 70
Felds experiment: A new flexible soft docking concept 69
Calibration activity of a sky quality meter for autonomous light pollution measurement 68
Large constellations assessment and optimization in LEO space debris environment 68
Dynamic behavior of a semi-androgynous small satellite docking interface 66
Deployment requirements for deorbiting electrodynamic tether technology 65
Kinematic tests on a docking mechanism for microsatellites 63
Measurement of light pollution and sky brightness in a sounding balloon flight: data elaboration through inertial pointing reconstruction. 62
Flight test of an autonomous payload for measuring sky brightness and ground light pollution using a stratospheric sounding balloon 62
Low-cost, high-resolution, self-powered, miniaturized sun sensor for space applications 61
Microgravity tests in preparation of a tethered electromagnetic docking space demonstration 61
SPACE DEBRIS REMOVAL USING MULTI-MISSION MODULAR SPACECRAFT 61
Conceptual design of a rechargeable air thruster for small aerial vehicles 60
CONCEPTUAL DESIGN OF SMALL SPACECRAFT DOCKING MECHANISM ACTUATED BY ELECTROACTIVE POLYMERS 60
Tethered electromagnetic capture: a cubesat mission concept 59
Test of tethered deorbiting of space debris 59
COLLISION AVOIDANCE MANEUVERS FOR SPACE TETHER SYSTEMS 59
Differential gps attitude determination concept for cubesats and drones 57
Multibody tether concept for asteroids capture 54
Preliminary observation of Marmolada glacier collapse of July 2022 with space-based cameras 53
LABORATORY VALIDATION OF CLOSE NAVIGATION, RENDEZVOUS AND DOCKING TECHNOLOGIES FOR NANOSATS 53
ERMES: Design and preliminary simulations for an autonomous docking manoeuvre 52
Proximity relative navigation sensors for small-scale spacecraft and drones 52
New Optical Communication Capabilities Using Nanosatellites 51
Polaris experiment: Stratospheric flight outcomes and experience gained from the rexus-bexus programme 51
Economic Value Proposition of Modular Assemblies 51
A NOVEL SEMI-EMPIRICAL TOOL FOR HYPERVELOCITY COLLISION SIMULATIONS 50
Atmospheric modeling by SCRAT experiment during the 2010 ESA BEXUS 10 Flight Campaign 50
Concept and feasibility analysis of the Alba CubeSat mission 50
Concept and Feasibility Analysis of the Alba Cubesat Mission 49
Investigation of ENVISAT catastrophic fragmentation scenarios 49
Experiment design of a payload for a sub-orbital rocket to study spacecraft repair after space debris impacts 49
O-ZONE: affordable stratospheric air dynamic sampling device 48
Overview of spacecraft fragmentation testing 46
Numerical simulations of hypervelocity collisions scenarios against a large satellite 46
A conceptual study to characterize properties of space debris from hypervelocity impacts through Thin Film Heat Flux Gauges 46
An overview of research activities at University of Padova in the field of satellite impacts with space debris 44
The ATEMO device: a reconfigurable system for Earth Monitoring and Observation 44
Technologies to join spacecraft using a tethered electromagnetic probe 44
Enabling ENVISAT deorbiting: a multi-spacecraft mission for inspection, capture, and detumbling 44
Experimental characterization of multi-layer 3D-printed shields for microsatellites 44
An overview on Smart Ballistic Optimization for Repairing of Aerospace Exostructures using 3D printed Kevlar 42
DAMPER DEVICE AND CONNECTING APPARATUS 42
Spacecraft joining using a tethered electromagnetic probe 42
O-ZONE: CFCs and PM dynamic sampling in the stratosphere 42
EXPERIMENTAL DETERMINATION OF MECHANICAL CHARACTERISTICS OF TAPES FOR SPACE APPLICATIONS 41
Development of a single-stage light-gas gun facility in Malta: a cooperative conceptual evaluation. 39
STAR: A UNIVERSITY STUDENTS DROP TOWER EXPERIMENT 39
Deployment Functional Tests of an Electrodynamic Tape for Space Debris Mitigation 39
Feasibility analysis of a CubeSat mission for Space Rider observation and docking 38
Impact risk assessment of deorbiting strategies in low earth orbits 38
Large constellations vulnerability assessment 37
CONJUGATING EDUCATIONAL ACTIVITIES AND TECHNOLOGY DEVELOPMENT: THE EXAMPLE OF TED PROJECT 35
Numerical evaluation of the influence of pre-arranged fault lines in the fragmentation of satellites subjected to hypervelocity collisions 35
An Overview of the Application of 3D Printed Spacecraft Structures within the ReDSHIFT Project 35
Totale 7.878
Salva come PNG Salva come JPEG
Categoria #
all - tutte 39.728
article - articoli 10.344
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 342
selected - selezionate 0
volume - volumi 270
Totale 50.684
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020246 0 0 0 0 0 0 0 49 44 55 87 11
2020/2021491 21 20 39 7 22 12 72 42 44 41 65 106
2021/20221.103 24 139 48 19 73 34 223 123 56 42 79 243
2022/20231.238 189 104 75 155 154 140 45 66 141 40 91 38
2023/20242.293 47 121 174 171 485 217 167 146 153 161 213 238
2024/20252.811 160 506 330 332 571 297 357 258 0 0 0 0
Totale 9.094