FRANCESCONI, ALESSANDRO
 Distribuzione geografica
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Continente #
NA - Nord America 8.580
EU - Europa 2.217
AS - Asia 1.332
OC - Oceania 18
SA - Sud America 18
AF - Africa 6
Continente sconosciuto - Info sul continente non disponibili 5
Totale 12.176
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Nazione #
US - Stati Uniti d'America 8.552
IT - Italia 1.102
CN - Cina 826
FI - Finlandia 272
DE - Germania 229
VN - Vietnam 180
JP - Giappone 140
GB - Regno Unito 135
SE - Svezia 127
UA - Ucraina 112
FR - Francia 64
IN - India 59
NL - Olanda 50
IE - Irlanda 37
HK - Hong Kong 27
CA - Canada 26
IR - Iran 19
KR - Corea 17
RU - Federazione Russa 17
SG - Singapore 14
BR - Brasile 12
AU - Australia 11
ES - Italia 11
BE - Belgio 10
TW - Taiwan 10
CH - Svizzera 9
TR - Turchia 8
NZ - Nuova Zelanda 7
ID - Indonesia 6
PH - Filippine 6
AE - Emirati Arabi Uniti 5
BG - Bulgaria 5
LU - Lussemburgo 5
MY - Malesia 5
EU - Europa 4
MT - Malta 4
AT - Austria 3
BD - Bangladesh 3
CO - Colombia 3
EG - Egitto 3
HU - Ungheria 3
LT - Lituania 3
PL - Polonia 3
PT - Portogallo 3
SK - Slovacchia (Repubblica Slovacca) 3
AL - Albania 2
CZ - Repubblica Ceca 2
IL - Israele 2
MA - Marocco 2
NO - Norvegia 2
PK - Pakistan 2
RO - Romania 2
A2 - ???statistics.table.value.countryCode.A2??? 1
AR - Argentina 1
CL - Cile 1
CR - Costa Rica 1
CY - Cipro 1
ET - Etiopia 1
MD - Moldavia 1
NP - Nepal 1
OM - Oman 1
PA - Panama 1
PE - Perù 1
SI - Slovenia 1
Totale 12.176
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Città #
Chandler 1.094
Fairfield 1.057
Woodbridge 770
Houston 686
Ann Arbor 624
Ashburn 556
Beijing 452
Jacksonville 433
Wilmington 421
Cambridge 407
Seattle 312
Padova 301
Princeton 224
Dong Ket 179
Medford 178
Des Moines 130
San Diego 122
Helsinki 116
Boardman 106
Osaka 102
Nanjing 90
Roxbury 88
Milan 87
Verona 60
Rome 41
Dublin 36
Lavis 34
Ogden 34
Hebei 33
Nanchang 31
Shenyang 30
Columbus 28
Norwalk 24
Redwood City 22
Guangzhou 19
New York 19
Shanghai 19
Washington 19
Badia Polesine 18
London 18
Venice 18
Jiaxing 17
Turin 17
Dallas 16
Pune 15
Tokyo 15
Falls Church 14
Vicenza 14
Changsha 13
Tianjin 13
Hong Kong 12
Indiana 12
Leiden 12
Council Bluffs 11
Kharkiv 11
Lappeenranta 11
Napoli 11
Ottawa 11
Pisa 11
Toronto 10
Cadoneghe 9
Tappahannock 9
Bibbiena 8
Borås 8
Dordrecht 8
Florence 8
Jinan 8
Monselice 8
Rio Rancho 8
Sao Jose 8
Torino 8
Zoetermeer 8
Chicago 7
Naples 7
Paris 7
Arzignano 6
Berlin 6
Brussels 6
Cavallino-Treporti 6
Central 6
Edinburgh 6
Lodi 6
Los Angeles 6
Moscow 6
Mumbai 6
Singapore 6
Taipei 6
Vittorio Veneto 6
Zhengzhou 6
Agordo 5
Brendola 5
Dresden 5
Dulles 5
Kilburn 5
Mirandola 5
Nottingham 5
Oxford 5
Robbiate 5
Tehran 5
Treviso 5
Totale 9.542
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Nome #
Fragments Distribution Prediction for ENVISAT Catastrophic Fragmentation 311
Space Rider Observer Cube – SROC: a CubeSat mission for proximity operations demonstration 266
A relative navigation sensor for CubeSats based on LED fiducial markers 140
ARCADE‑R2 EXPERIMENT ON BOARD BEXUS 17 STRATOSPHERIC BALLOON 136
Development of a low-cost sun sensor for nanosatellites 135
Impact facility based upon high frequency two stage light-gas gun 129
Active debris multi-removal mission concept based on hybrid propulsion 126
Design, qualification, and acceptance of the front door mechanisms for the OSIRIS experiment of Rosetta mission 124
Impact Risk Analysis for a Spacecraft in Cosmo-Skymed Orbit 122
Cubesat mission concept for tethered electromagnetic docking demonstration 122
DESIGN OF DOCKING MECHANISM FOR SMALL SPACECRAFT 119
2D Close-Range Navigation Sensor for Miniature Cooperative Spacecraft 119
A contribution to the definition of a new method to predict the catastrophic disintegration of spacecraft after collision with large orbital debris 115
A system to damp the free piston oscillations in a two-stage light-gas gun used for hypervelocity impact experiments 114
TED project: Conjugating technology development and educational activities 113
Hypervelocity experiments of impact cratering and catastrophic disruption of targets representative of minor bodies of the Solar System 112
A special design condition to increase the performance of two-stage light-gas guns 111
Active piston technique to optimize the chamber pressure in two-stage light-gas guns 108
High Precision Dual-Stage Pointing Mechanism for Miniature Satellite Laser Communication Terminals 108
An innovative space tether deployer with retrieval capability: design and test of star experiment 108
Analysis of transient vibrations on complex targets representing elementary configurations of GOCE satellite 107
CST: A new semi-empirical tool for simulating spacecraft collisions in orbit 106
Design of an innovative Dielectric Elastomer actuator for space applications 102
CST: a new semi-empirical tool for simulating spacecraft collisions in orbit 102
Acceleration fields induced by hypervelocity impacts on spacecraft structures" International Journal of Impact Engineering 99
Active space debris removal by a hybrid propulsion module 99
A STUDENT EXPERIMENT FROM STRATOSPHERIC BALLOON BEXUS 10: SCRAT FROM CONCEPT TO LAUNCH 98
LaserCube optical communication terminal for nano and micro satellites 98
An engineering model to describe fragments clouds propagating inside spacecraft in consequence of space debris impact on sandwich panel structures 96
Acceleration fields induced by hypervelocity impacts on spacecraft structures 96
Effect of hypervelocity impact on microcellular ceramic foams from a preceramic polymer 96
Survivability to orbital debris of tape tethers for end-of-life spacecraft de-orbiting 96
Modelling and control of double-cone dielectric elastomer actuator 96
SPH evaluation of out-of-plane peak force transmitted during a hypervelocity impact 94
Experimental evaluation of a Dielectric Elastomer robotic arm for space applications 94
Experimental Investigation of the Ballistic Response of Composite Panels Coupled with a Self-Healing Polymeric Layer 94
KINEMATICS AND CONTROL OF REDUNDANT ROBOTIC ARM BASED ON DIELECTRIC ELASTOMER ACTUATORS 93
Improvement of the CISAS high-shot-frequency light-gas gun 92
An estimation method for the Shock Response Spectrum propagating into plates subjected to hypervelocity impact 92
A new ballistic limit equation for thin tape tethers 92
Design and test in microgravity of a space tether length and length rate measurement device 92
Comparison of self-healing ionomer to aluminium-alloy bumpers for protecting spacecraft equipment from space debris impacts 90
An engineering model to describe fragments clouds propagating inside spacecraft in consequence of space debris impact on sandwich panel structures 90
Selecting materials to protect inflatable structures from the space environment 88
Impact experiments on low-temperature bumpers 87
Effects of high-speed impacts on CFRP plates for space applications 85
Application of Wavelet Transform to analyze acceleration signals generated by HVI on thin aluminum plates and all-aluminum honeycomb sandwich panels 84
ERMES: Experimental Rendezvous in Microgravity Environment Study 84
A miniature stabilized platform for lasercom terminals on-board nanosatellites 79
Impact facility based upon high frequency two stage light-gas gun. 78
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 78
Autoport project: A docking station for planetary exploration drones 76
Debris Impact on CFRP-AL Honeycomb Sandwich Structure 75
A New Set-Up to Investigate Plastic Deformation of Face Centered Cubic Metals in High Strain Rate Loading 75
Impact facility based upon high frequency two stage light-gas gun 74
Large debris removal mission in LEO based on hybrid propulsion 74
Ballistic Limit of CFRP Plates 73
End-of-life deorbiting services for small satellites making use of bare electrodynamic tethers 73
Mini launcher vehicle University program Based on Hybrid propulsion 71
Direct temperature measurements during Netlander descent on MARS 70
A new concept variable resistance radiator 70
A new concept of variable resistance radiator: Stratospheric flight test and performance analysis 70
e.Cube Mission: the Environmental CubeSat 70
An experimental study of the self-healing behavior of ionomeric systems under ballistic impact tests 68
Autonomous Rendezvous, Control and Docking Experiment – Reflight 2 68
Semi-androgynous multifunctional interface for expandable space structures 68
A relative navigation sensor for CubeSats based on retro-reflective markers 68
Generation of transient vibrations on aluminum honeycomb sandwich panels subjected to hypervelocity impacts 68
Collision-Avoidance Maneuvers for a satellite Pair Flying in Tight Formation 67
Design and test of a semiandrogynous docking mechanism for small satellites 66
Arcade experiment on board bexus 13 and 17: Design, integration and flight of a technology test platform within a student balloon programme 66
Effect of honeycomb core under hypervelocity impact: Numerical simulation and engineering model 66
Miniature docking mechanism for CubeSats 66
Low-cost relative navigation sensors for miniature spacecraft and drones 65
Large constellations assessment and optimization in LEO space debris environment 63
Rate-dependent self-healing behavior of an ethylene-co-methacrylic acid ionomer under high-energy impact conditions 62
A new Ballistic Limit Equation for thin tape tethers 62
Dynamic analysis of thin-film solar panels in LEO 62
Morphing electroadhesive interface to manipulate uncooperative objects 60
Hypervelocity Impacts on Dyneema Ropes 60
A method to assess the average properties of spacecraft ejecta from hypervelocity impact 59
Data retrieved by SCRAT experiment during the 2010 ESA BEXUS 10 flight campaign 59
INNOVATIVE TECHNOLOGIES FOR NON-COOPERATIVE TARGETS CLOSE INSPECTION AND GRASPING 56
Active debris removal space mission concepts based on hybrid propulsion 56
Flexible electromagnetic leash docking system (felds) experiment from design to microgravity testing 55
Tethered electromagnetic capture: a cubesat mission concept 55
Differential gps attitude determination concept for cubesats and drones 55
Low-cost, high-resolution, self-powered, miniaturized sun sensor for space applications 54
Development and test of a robotic arm for experiments on close proximity operations 53
High velocity impact behavior of composite sandwich panels with self-healing capabilities 52
Ground Facility for Validation of Proximity Operations: a Hardware–In–the–Loop Experiment 52
Numerical formulation of the equations describing the rigid-body dynamics of a variable mass rocket with internal flow 51
Misure di accelerazione su campioni sottoposti ad impatto iperveloce: caratterizzazione del rumore di fondo della CISAS Impact Facility 50
Fast and Accurate Numerical Integration of Relative Motion in Spacecraft Formation Flying 50
Laboratory impact experiments on rocky and icy surface:variation effects of the physical properties of the surface of Solar System bodies 50
Numerical simulations on a smart control systems for membrane structures 50
SPACE DEBRIS REMOVAL USING MULTI-MISSION MODULAR SPACECRAFT 50
Felds experiment: A new flexible soft docking concept 50
Conceptual design of a rechargeable air thruster for small aerial vehicles 49
ACTIVE SPACE DEBRIS REMOVAL BY HYBRID ENGINE MODULE 49
Totale 8.646
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Categoria #
all - tutte 41.438
article - articoli 15.610
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 588
patent - brevetti 73
selected - selezionate 0
volume - volumi 81
Totale 57.790
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019518 0 0 0 0 0 0 0 0 0 116 220 182
2019/20201.839 303 56 13 141 167 129 137 197 171 230 206 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
2023/20242.011 97 190 230 172 497 234 193 177 151 70 0 0
Totale 12.408