BARATO, FRANCESCO
 Distribuzione geografica
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Continente #
NA - Nord America 6.176
AS - Asia 4.499
EU - Europa 2.608
AF - Africa 735
SA - Sud America 678
OC - Oceania 80
Continente sconosciuto - Info sul continente non disponibili 24
Totale 14.800
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Nazione #
US - Stati Uniti d'America 5.801
SG - Singapore 1.335
IT - Italia 822
CN - Cina 812
VN - Vietnam 586
HK - Hong Kong 444
BR - Brasile 384
DE - Germania 260
IN - India 192
FR - Francia 182
NL - Olanda 162
GB - Regno Unito 156
FI - Finlandia 139
TR - Turchia 109
PL - Polonia 88
BD - Bangladesh 86
JP - Giappone 85
SE - Svezia 82
CA - Canada 73
RU - Federazione Russa 70
CI - Costa d'Avorio 66
IQ - Iraq 66
AR - Argentina 62
TW - Taiwan 61
ES - Italia 52
UA - Ucraina 49
PH - Filippine 48
PK - Pakistan 48
ID - Indonesia 47
SA - Arabia Saudita 45
KR - Corea 44
MX - Messico 39
BJ - Benin 38
IE - Irlanda 36
PT - Portogallo 36
ZA - Sudafrica 36
CO - Colombia 34
UZ - Uzbekistan 34
EC - Ecuador 33
AT - Austria 31
AE - Emirati Arabi Uniti 30
CL - Cile 30
IL - Israele 30
PY - Paraguay 30
BE - Belgio 29
MA - Marocco 29
NP - Nepal 29
TH - Thailandia 29
AZ - Azerbaigian 26
DZ - Algeria 26
UY - Uruguay 26
AU - Australia 25
VE - Venezuela 25
AO - Angola 24
IR - Iran 24
MY - Malesia 24
CH - Svizzera 23
CR - Costa Rica 23
LB - Libano 23
NO - Norvegia 23
RO - Romania 23
BO - Bolivia 22
CZ - Repubblica Ceca 22
GN - Guinea 22
MN - Mongolia 22
AM - Armenia 21
ET - Etiopia 21
JM - Giamaica 21
JO - Giordania 21
KE - Kenya 21
KZ - Kazakistan 21
LY - Libia 21
NI - Nicaragua 21
TN - Tunisia 21
BF - Burkina Faso 20
BY - Bielorussia 20
LV - Lettonia 20
RS - Serbia 20
SK - Slovacchia (Repubblica Slovacca) 20
SN - Senegal 20
DK - Danimarca 19
HN - Honduras 19
HT - Haiti 19
AD - Andorra 18
CM - Camerun 18
HR - Croazia 18
HU - Ungheria 18
IS - Islanda 18
MD - Moldavia 18
UG - Uganda 18
BA - Bosnia-Erzegovina 17
CV - Capo Verde 17
GA - Gabon 17
LA - Repubblica Popolare Democratica del Laos 17
MR - Mauritania 17
PE - Perù 17
RE - Reunion 17
YT - Mayotte 17
BB - Barbados 16
GR - Grecia 16
Totale 14.072
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Città #
San Jose 758
Singapore 755
Fairfield 598
Ashburn 569
Hong Kong 391
Chandler 332
Woodbridge 288
Seattle 260
Wilmington 230
Houston 227
Cambridge 205
Beijing 200
Ann Arbor 189
Ho Chi Minh City 189
Santa Clara 187
Hanoi 142
New York 135
Los Angeles 126
Boardman 111
Rome 89
Padova 81
Lauterbourg 69
Medford 69
Princeton 69
Chicago 67
Milan 64
Abidjan 63
Helsinki 63
Munich 60
San Diego 59
Des Moines 58
Bytom 49
Roxbury 45
São Paulo 43
Orem 39
Cotonou 37
Tokyo 37
Turku 35
London 34
Buffalo 32
Turin 32
Naples 30
Tashkent 30
Frankfurt am Main 29
Dublin 28
Nanjing 28
Redondo Beach 27
Haiphong 26
Baghdad 25
Vienna 25
Council Bluffs 24
Guangzhou 24
Montreal 24
Baku 23
Dallas 23
Falkenstein 23
Istanbul 23
Warsaw 23
Amsterdam 22
Chennai 22
Salt Lake City 22
Amman 21
Luanda 21
Managua 21
Montevideo 21
Stockholm 21
Ulan Bator 21
Addis Ababa 20
Da Nang 20
Dakar 20
Conakry 19
Lahore 19
Mumbai 19
Tainan City 19
Yerevan 19
Andorra la Vella 18
Ankara 18
Atlanta 18
Jeddah 18
Kampala 17
Riga 17
Tripoli 17
Denver 16
Libreville 16
Vientiane 16
Bridgetown 15
Johannesburg 15
Nairobi 15
Nouakchott 15
Riyadh 15
Toronto 15
Abu Dhabi 14
Phnom Penh 14
Phoenix 14
Praia 14
Rio de Janeiro 14
Zagreb 14
Asunción 13
Biên Hòa 13
Brooklyn 13
Totale 8.252
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Nome #
Numerical and Experimental Investigation of Hybrid Rocket Motors Transient Behavior 557
Design and In-orbit Demonstration of REGULUS, an Iodine electric propulsion system 306
The "Vortex Reloaded" project: numerical investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 292
Correction to: Design and Testing of a 3D Printed Regenerative Cooled Nozzle for a Hydrogen Peroxide based Bi-Propellant Thruster (AIAA Propulsion and Energy Forum, 2021) 269
CFD Simulation of a Hybrid Rocket Motor with Liquid Injection 253
Investigation of different strategies for access to space of small satellites on a defined LEO orbit 251
Numerical Modeling of Paraffin-Based Fuels Behavior 251
Modeling and CFD Simulation of Regression Rate in Hybrid Rocket Motors 249
Testing of a Long-Burning-Time Paraffin-Based Hybrid Rocket Motor 242
Numerical Model to Analyze Transient Behavior and Instabilities on Hybrid Rocket Motors 241
Scaling Parameters of Swirling Oxidizer Injection in Hybrid Rocket Motors 238
Real-Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor 236
Design and Testing of a 3D Printed 10 N Hydrogen Peroxide Monopropellant Thruster 235
SPONGE: a Sounding Rocket Experiment for PMDs 230
Regression Rate Design Tailoring Through Vortex Injection in Hybrid Rocket Motors 220
Development of a Flow Control Valve for a Throttleable Hybrid Rocket Motor and Throttling Fire Tests 219
Design and testing of a hydrogen peroxide bipropellant thruster 219
Investigation of Effect of Diaphragms on the Efficiency of Hybrid Rockets 218
Numerical and Experimental Investigation on Vortex Injection in Hybrid Rocket Motors 211
A numerical model to analyze the transient behavior and instabilities on hybrid rocket motors 208
Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection - Part 2 206
The SPONGE rexus project: Overview of a sounding rocket experiment for PMDs 203
REGULUS: INTEGRATION AND TESTING OF AN IODINE ELECTRIC PROPULSION SYSTEM 203
Numerical analyses of thermal protection design in hybrid rocket motors 201
Update on green chemical propulsion activities and achievements by the University of Padua and its spin-off T4I 200
Development and Testing of a Long Burning Time Lab-scale Paraffin-Based Hybrid Rocket Motor 200
REGULUS: Know-How Acquired on Iodine Propellant 200
REGULUS: Iodine Fed Plasma Propulsion System for Small Satellites 199
Numerical Investigation of Hybrid Motors for the EU FP7 SPARTAN Program 196
Numerical and Experimental Investigation of Unidirectional Vortex Injection in Hybrid Rocket Engines 193
A Simplified Thermal Analysis Model for Regeneratively Cooled Rocket Engine Thrust Chambers and Its Calibration with Experimental Data 189
Status and Achievements of the Hydrogen Peroxide Chemical Propulsion Research at Padua University 189
Numerical Simulation of an Isochoric Combustion Chamber for Hybrid Rocket Propulsion 188
Computational Fluid Dynamics Simulation of Regression Rate in Hybrid Rockets 185
CFD Simulations of Self-Pressurized Nitrous Oxide Hybrid Rocket Motors 185
Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection 184
Impact of propulsion system characteristics on the potential for cost reduction of earth observation missions at very low altitudes 183
Development and testing of an engineering model of a hydrogen peroxide based 1N propulsion unit 182
Design and Testing of a 3D Printed Regenerative Cooled Nozzle for a Hydrogen Peroxide based Bi-Propellant Thruster 182
Numerical Investigation of Hybrid Rocket Combustion Chamber Transient Behavior 181
Integrated approach for hybrid rocket technology development 179
The "Vortex Reloaded" project: experimental investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 177
Challenges of ablatively cooled hybrid rockets for satellites or upper stages 171
Explicit analytical equations for single port hybrid rocket combustion chamber sizing 169
Computational fluid dynamics simulation of hybrid rockets of different scales 161
CONCEPTUAL DESIGN OF THE ELECTRIC PUMPS FOR THE HIGH-PERFORMANCE ENGINE OF A EUROPEAN LUNAR LANDER 160
Development of a Cavitating Pintle for a Throttleable Hybrid Rocket Motor 156
Analysis of Fluid-dynamic Systems to Increase Combustion Efficiency in Hybrid Rockets 155
Explicit Analytical Equations for Single Port Hybrid Rocket Combustion Chamber Sizing 154
Numerical simulation of hybrid rockets liquid injection and comparison with experiments 153
Numerical and Experimental Activities in Support of the Development of Hybrid Rocket Engine for Soft-Landing Applications 152
Real-Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor 150
Comparison between Different Re-Entry Technologies for Debris Mitigation in LEO 149
Numerical Model to Analyse Nozzle Termochemical Erosion 145
CFD Simulation of Regression Rate in Hybrid Rockets 144
Testing and CFD simulation of diaphragm hybrid rocket motors 141
Integrated approach for hybrid rocket technology development 141
Testing and CFD Simulation of Diaphragm Hybrid Rocket Motors 139
Numerical and Experimental Activities in Support of the Development of Hybrid-Rocket Engine for softlanding applications 139
Development of the Propulsion System for a Moon Drone Vehicle Demonstrator 136
Experimental Investigation of a H2O2 Hybrid Rocket with Different Swirl Injections and Fuels 135
Numerical Investigation of Pressure-Fed Solutions for Paraffin-Based Hybrid Rocket Motors 135
Numerical Simulations of an H2O2 Vortex Hybrid Rocket Motor 134
C/C-SiC Nozzle for a Long Burn-Time Hybrid Rocket: Design and Optimization, Manufacturing and Testing 133
Review of Alternative Sustainable Fuels for Hybrid Rocket Propulsion 132
Magnetic Enhanced Plasma Propulsion System for small-satellites IOD development 132
Numerical Simulations of an Isochoric Hybrid Rocket Combustion Chamber and Comparison with Tests 127
Numerical optimization of hybrid sounding rockets through coupled motor-trajectory simulation 125
Electric propulsion technology for low earth mission of micro/nano-satellites 124
Preliminary Design of the Propulsion Subsystem for the European Advanced Reusable Satellite (EARS) 120
Optimal use of electric propulsion for drag compensation in very low earth orbit on satellites with deployable solar panels 119
Numerical Simulations of a Paraffin-Hydrogen Peroxide Hybrid Rocket with Swirl Injection 119
Investigation of different strategies for access to space of small satellites on a defined LEO orbit 118
Variations and Control of Thrust and Mixture Ratio in Hybrid Rocket Motors 117
CFD Simulation in Support of SPARTAN Research Program 116
Preliminary Design of the European Advanced Reusable Satellite EARS 116
Variations and Control of Thrust and Mixture Ratio in Hybrid Rocket Motors 113
Investigation of the influence of gas phase molecular mass variations on hybrid rocket regression rate 108
Hybrid rocket residuals - An overlooked topic 108
Testing of a Small HTP Monopropellant Thruster for Space Applications 95
Hybrid Rocket Motor Regression Rate Prediction trough CFD Simulations 94
Impact of propulsion system characteristics on the potential for cost reduction of earth observation missions at very low altitudes 91
OPTIMAL USE OF ELECTRIC PROPULSION FOR DRAG COMPENSATION IN VERY LOW EARTH ORBIT ON SATELLITES WITH DEPLOYABLE SOLAR PANELS 88
Ascent Trajectory Optimisation for Hybrid Propulsion Micro Launcher 85
Development and Test of an Innovative Hybrid Rocket Combustion Chamber 80
Totale 14.929
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Categoria #
all - tutte 40.324
article - articoli 12.087
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 52.411
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021182 0 0 0 0 0 0 0 0 0 0 98 84
2021/2022806 17 97 56 23 75 35 20 74 77 48 88 196
2022/2023814 124 75 18 85 143 110 8 53 82 34 62 20
2023/2024648 25 62 28 75 52 90 37 71 28 50 66 64
2024/20252.319 18 137 102 123 243 121 103 235 219 73 373 572
2025/20268.007 345 561 1.072 1.402 949 331 906 923 746 474 298 0
Totale 14.929