FRANCESCONI, ALESSANDRO
 Distribuzione geografica
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Continente #
NA - Nord America 9.680
EU - Europa 3.339
AS - Asia 2.602
SA - Sud America 37
OC - Oceania 28
AF - Africa 12
Continente sconosciuto - Info sul continente non disponibili 5
Totale 15.703
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Nazione #
US - Stati Uniti d'America 9.636
IT - Italia 1.742
CN - Cina 1.079
SG - Singapore 793
DE - Germania 292
FI - Finlandia 284
FR - Francia 232
JP - Giappone 190
VN - Vietnam 184
GB - Regno Unito 180
SE - Svezia 132
IN - India 128
UA - Ucraina 112
NL - Olanda 98
RU - Federazione Russa 72
HK - Hong Kong 52
KR - Corea 44
IE - Irlanda 43
CA - Canada 38
ES - Italia 32
IR - Iran 32
PH - Filippine 25
AU - Australia 21
BR - Brasile 17
BE - Belgio 16
PT - Portogallo 16
LU - Lussemburgo 14
TR - Turchia 14
CH - Svizzera 13
MT - Malta 12
PE - Perù 12
TW - Taiwan 12
PL - Polonia 11
ID - Indonesia 10
MY - Malesia 10
NZ - Nuova Zelanda 7
BD - Bangladesh 6
BG - Bulgaria 6
AE - Emirati Arabi Uniti 5
EG - Egitto 5
HU - Ungheria 5
IQ - Iraq 5
AT - Austria 4
CZ - Repubblica Ceca 4
EU - Europa 4
IL - Israele 4
MA - Marocco 4
CO - Colombia 3
LT - Lituania 3
MX - Messico 3
OM - Oman 3
PK - Pakistan 3
SI - Slovenia 3
SK - Slovacchia (Repubblica Slovacca) 3
AL - Albania 2
AR - Argentina 2
CL - Cile 2
DK - Danimarca 2
NO - Norvegia 2
RO - Romania 2
A2 - ???statistics.table.value.countryCode.A2??? 1
BA - Bosnia-Erzegovina 1
BO - Bolivia 1
CR - Costa Rica 1
CY - Cipro 1
DO - Repubblica Dominicana 1
ET - Etiopia 1
MD - Moldavia 1
NG - Nigeria 1
NP - Nepal 1
PA - Panama 1
TM - Turkmenistan 1
ZA - Sudafrica 1
Totale 15.703
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Città #
Chandler 1.094
Fairfield 1.057
Woodbridge 770
Houston 686
Singapore 656
Ann Arbor 624
Ashburn 608
Beijing 471
Boardman 446
Jacksonville 433
Padova 427
Wilmington 421
Cambridge 411
Santa Clara 317
Seattle 312
Princeton 224
Dong Ket 179
Medford 178
Milan 151
Des Moines 130
Helsinki 122
San Diego 122
Osaka 106
Nanjing 94
Roxbury 88
Rome 73
Verona 66
Turin 60
Dublin 41
Lavis 34
Ogden 34
Hebei 33
Nanchang 33
Venice 33
Hong Kong 30
Shenyang 30
Columbus 28
Dallas 28
Tokyo 28
Shanghai 25
Norwalk 24
Reggio Emilia 24
Guangzhou 23
Naples 23
Vicenza 23
New York 22
Redwood City 22
Pisa 21
London 19
Munich 19
Washington 19
Badia Polesine 18
Los Angeles 18
Paese 18
Jiaxing 17
Leiden 16
Bengaluru 15
Changsha 15
Jinan 15
Mumbai 15
Pune 15
Falls Church 14
Lappeenranta 14
Newton 14
Treviso 14
Iloilo City 13
Madrid 13
San Jose 13
Tianjin 13
Indiana 12
Council Bluffs 11
Kharkiv 11
Kochi 11
Lima 11
Napoli 11
Nottingham 11
Ottawa 11
Toronto 11
Trieste 11
Budrio 10
Chicago 10
Florence 10
Hengyang 10
Leicester 10
Moscow 10
Tehran 10
Bologna 9
Cadoneghe 9
Frankfurt am Main 9
Paris 9
Santo Tirso 9
Tappahannock 9
Bibbiena 8
Borås 8
Braunschweig 8
Brussels 8
Dordrecht 8
Genoa 8
Luxembourg 8
Melbourne 8
Totale 11.511
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Nome #
Space Rider Observer Cube – SROC: a CubeSat mission for proximity operations demonstration 458
Fragments Distribution Prediction for ENVISAT Catastrophic Fragmentation 336
DESIGN OF DOCKING MECHANISM FOR SMALL SPACECRAFT 309
A relative navigation sensor for CubeSats based on LED fiducial markers 148
Development of a low-cost sun sensor for nanosatellites 145
ARCADE‑R2 EXPERIMENT ON BOARD BEXUS 17 STRATOSPHERIC BALLOON 143
Impact facility based upon high frequency two stage light-gas gun 140
Active debris multi-removal mission concept based on hybrid propulsion 136
Design, qualification, and acceptance of the front door mechanisms for the OSIRIS experiment of Rosetta mission 133
CST: A new semi-empirical tool for simulating spacecraft collisions in orbit 133
2D Close-Range Navigation Sensor for Miniature Cooperative Spacecraft 130
Cubesat mission concept for tethered electromagnetic docking demonstration 129
An innovative space tether deployer with retrieval capability: design and test of star experiment 129
Impact Risk Analysis for a Spacecraft in Cosmo-Skymed Orbit 128
A contribution to the definition of a new method to predict the catastrophic disintegration of spacecraft after collision with large orbital debris 125
A system to damp the free piston oscillations in a two-stage light-gas gun used for hypervelocity impact experiments 123
A special design condition to increase the performance of two-stage light-gas guns 121
Hypervelocity experiments of impact cratering and catastrophic disruption of targets representative of minor bodies of the Solar System 121
CST: a new semi-empirical tool for simulating spacecraft collisions in orbit 120
Active piston technique to optimize the chamber pressure in two-stage light-gas guns 119
High Precision Dual-Stage Pointing Mechanism for Miniature Satellite Laser Communication Terminals 117
Analysis of transient vibrations on complex targets representing elementary configurations of GOCE satellite 116
TED project: Conjugating technology development and educational activities 116
LaserCube optical communication terminal for nano and micro satellites 114
A STUDENT EXPERIMENT FROM STRATOSPHERIC BALLOON BEXUS 10: SCRAT FROM CONCEPT TO LAUNCH 112
Design of an innovative Dielectric Elastomer actuator for space applications 112
e.Cube Mission: the Environmental CubeSat 112
Improvement of the CISAS high-shot-frequency light-gas gun 111
ERMES: Experimental Rendezvous in Microgravity Environment Study 111
An engineering model to describe fragments clouds propagating inside spacecraft in consequence of space debris impact on sandwich panel structures 107
Acceleration fields induced by hypervelocity impacts on spacecraft structures 107
A new ballistic limit equation for thin tape tethers 107
Acceleration fields induced by hypervelocity impacts on spacecraft structures" International Journal of Impact Engineering 106
Active space debris removal by a hybrid propulsion module 106
Modelling and control of double-cone dielectric elastomer actuator 103
KINEMATICS AND CONTROL OF REDUNDANT ROBOTIC ARM BASED ON DIELECTRIC ELASTOMER ACTUATORS 103
An estimation method for the Shock Response Spectrum propagating into plates subjected to hypervelocity impact 102
An engineering model to describe fragments clouds propagating inside spacecraft in consequence of space debris impact on sandwich panel structures 102
Experimental Investigation of the Ballistic Response of Composite Panels Coupled with a Self-Healing Polymeric Layer 102
Survivability to orbital debris of tape tethers for end-of-life spacecraft de-orbiting 101
SPH evaluation of out-of-plane peak force transmitted during a hypervelocity impact 100
Effect of hypervelocity impact on microcellular ceramic foams from a preceramic polymer 99
AlbaSat: an educational satellite for a multi-objective mission in LEO 98
Design and test in microgravity of a space tether length and length rate measurement device 97
Experimental evaluation of a Dielectric Elastomer robotic arm for space applications 96
Comparison of self-healing ionomer to aluminium-alloy bumpers for protecting spacecraft equipment from space debris impacts 95
Selecting materials to protect inflatable structures from the space environment 93
Impact experiments on low-temperature bumpers 93
A miniature stabilized platform for lasercom terminals on-board nanosatellites 92
Advances in the characterisation of collision break-ups by means of numerical modelling 92
End-of-life deorbiting services for small satellites making use of bare electrodynamic tethers 91
Application of Wavelet Transform to analyze acceleration signals generated by HVI on thin aluminum plates and all-aluminum honeycomb sandwich panels 90
A novel approach to the simulation of on-orbit rendezvous and docking maneuvers in a laboratory environment through the aid o fan anthropomorphic robotic arm 90
Effects of high-speed impacts on CFRP plates for space applications 89
A New Set-Up to Investigate Plastic Deformation of Face Centered Cubic Metals in High Strain Rate Loading 88
Mini launcher vehicle University program Based on Hybrid propulsion 86
Ballistic Limit of CFRP Plates 82
Impact facility based upon high frequency two stage light-gas gun. 82
A new concept variable resistance radiator 82
A CubeSat-sized space debris impact sensor 82
Collision-Avoidance Maneuvers for a satellite Pair Flying in Tight Formation 81
Autonomous Rendezvous, Control and Docking Experiment – Reflight 2 81
A new concept of variable resistance radiator: Stratospheric flight test and performance analysis 81
Impact facility based upon high frequency two stage light-gas gun 81
Autoport project: A docking station for planetary exploration drones 80
ALBASAT: AN EDUCATIONAL SATELLITE FOR A MULTI-OBJECTIVES MISSION IN LEO 79
Debris Impact on CFRP-AL Honeycomb Sandwich Structure 79
A relative navigation sensor for CubeSats based on retro-reflective markers 78
Large debris removal mission in LEO based on hybrid propulsion 77
Development and test of a robotic arm for experiments on close proximity operations 77
An experimental study of the self-healing behavior of ionomeric systems under ballistic impact tests 76
Semi-androgynous multifunctional interface for expandable space structures 76
Miniature docking mechanism for CubeSats 76
Direct temperature measurements during Netlander descent on MARS 75
INNOVATIVE TECHNOLOGIES FOR NON-COOPERATIVE TARGETS CLOSE INSPECTION AND GRASPING 75
Generation of transient vibrations on aluminum honeycomb sandwich panels subjected to hypervelocity impacts 74
A new Ballistic Limit Equation for thin tape tethers 73
Towards In-Orbit Demonstration of a Compact Optical Communications Terminal for Small Satellites 73
Arcade experiment on board bexus 13 and 17: Design, integration and flight of a technology test platform within a student balloon programme 72
Ground Facility for Validation of Proximity Operations: a Hardware–In–the–Loop Experiment 72
Data retrieved by SCRAT experiment during the 2010 ESA BEXUS 10 flight campaign 71
An analitycal method for the propagation towards internal components of debris clouds originated by space debris impacts on spacecraft walls 71
Dynamic analysis of thin-film solar panels in LEO 71
A method to assess the average properties of spacecraft ejecta from hypervelocity impact 70
High velocity impact behavior of composite sandwich panels with self-healing capabilities 70
Design and test of a semiandrogynous docking mechanism for small satellites 70
Flexible electromagnetic leash docking system (felds) experiment from design to microgravity testing 70
Hypervelocity Impacts on Dyneema Ropes 70
Low-cost relative navigation sensors for miniature spacecraft and drones 69
Examination of satellite collision scenarios spanning low to hypervelocity encounters using semi-empirical models 69
Satellite and robotic arm combined control for spacecraft close-proximity operations 68
Effect of honeycomb core under hypervelocity impact: Numerical simulation and engineering model 68
Rate-dependent self-healing behavior of an ethylene-co-methacrylic acid ionomer under high-energy impact conditions 67
Active debris removal space mission concepts based on hybrid propulsion 67
Felds experiment: A new flexible soft docking concept 67
Large constellations assessment and optimization in LEO space debris environment 66
Overview of the AlbaSat mission the first CubeSat from University of Padova 65
Morphing electroadhesive interface to manipulate uncooperative objects 65
Fast and Accurate Numerical Integration of Relative Motion in Spacecraft Formation Flying 64
Numerical simulations on a smart control systems for membrane structures 61
Totale 10.205
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Categoria #
all - tutte 59.931
article - articoli 20.492
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 798
patent - brevetti 112
selected - selezionate 0
volume - volumi 160
Totale 81.493
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20201.159 0 0 0 0 0 129 137 197 171 230 206 89
2020/20211.553 50 93 50 88 58 141 72 138 209 146 205 303
2021/20221.989 37 379 194 57 83 92 103 201 111 59 171 502
2022/20232.512 422 270 97 294 338 292 34 151 272 75 186 81
2023/20242.692 97 190 230 172 497 234 193 177 151 181 242 328
2024/20252.890 214 605 462 434 852 323 0 0 0 0 0 0
Totale 15.979