BARATO, FRANCESCO
 Distribuzione geografica
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Continente #
NA - Nord America 6.590
AS - Asia 4.640
EU - Europa 2.778
AF - Africa 744
SA - Sud America 693
OC - Oceania 80
Continente sconosciuto - Info sul continente non disponibili 24
Totale 15.549
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Nazione #
US - Stati Uniti d'America 6.184
SG - Singapore 1.357
IT - Italia 949
CN - Cina 826
VN - Vietnam 592
HK - Hong Kong 452
BR - Brasile 390
DE - Germania 270
IN - India 200
FR - Francia 193
NL - Olanda 166
GB - Regno Unito 159
BD - Bangladesh 142
FI - Finlandia 142
TR - Turchia 110
JP - Giappone 90
CA - Canada 88
PL - Polonia 88
SE - Svezia 82
RU - Federazione Russa 71
TW - Taiwan 71
CI - Costa d'Avorio 66
IQ - Iraq 66
AR - Argentina 63
ES - Italia 52
UA - Ucraina 50
KR - Corea 48
PH - Filippine 48
PK - Pakistan 48
ID - Indonesia 47
SA - Arabia Saudita 45
MX - Messico 40
PT - Portogallo 40
BJ - Benin 38
CO - Colombia 37
IE - Irlanda 37
ZA - Sudafrica 36
UZ - Uzbekistan 35
EC - Ecuador 33
AT - Austria 32
CL - Cile 32
IL - Israele 32
AE - Emirati Arabi Uniti 30
NP - Nepal 30
PY - Paraguay 30
BE - Belgio 29
MA - Marocco 29
TH - Thailandia 29
AZ - Azerbaigian 26
DZ - Algeria 26
UY - Uruguay 26
VE - Venezuela 26
AU - Australia 25
CR - Costa Rica 25
AO - Angola 24
IR - Iran 24
LB - Libano 24
MY - Malesia 24
CH - Svizzera 23
GN - Guinea 23
JM - Giamaica 23
NO - Norvegia 23
RO - Romania 23
BO - Bolivia 22
CZ - Repubblica Ceca 22
MN - Mongolia 22
AM - Armenia 21
ET - Etiopia 21
HN - Honduras 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
AD - Andorra 19
DK - Danimarca 19
HR - Croazia 19
HT - Haiti 19
PE - Perù 19
BA - Bosnia-Erzegovina 18
CM - Camerun 18
HU - Ungheria 18
IS - Islanda 18
MD - Moldavia 18
RE - Reunion 18
UG - Uganda 18
BB - Barbados 17
CV - Capo Verde 17
GA - Gabon 17
LA - Repubblica Popolare Democratica del Laos 17
MR - Mauritania 17
YT - Mayotte 17
EG - Egitto 16
Totale 14.803
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Città #
San Jose 784
Singapore 773
Fairfield 604
Ashburn 599
Hong Kong 396
Chandler 337
Woodbridge 289
Seattle 263
Wilmington 231
Houston 230
Santa Clara 210
Cambridge 206
Beijing 202
Ho Chi Minh City 190
Ann Arbor 189
New York 145
Hanoi 142
Los Angeles 132
Boardman 127
Rome 104
Milan 82
Padova 81
Chicago 74
Lauterbourg 70
Medford 70
Princeton 70
Helsinki 65
Abidjan 63
San Diego 62
Munich 60
Des Moines 58
Naples 52
Bytom 49
Roxbury 46
São Paulo 43
Orem 41
Tokyo 39
Buffalo 37
Cotonou 37
Turin 36
Turku 36
London 34
Frankfurt am Main 32
Tashkent 31
Dallas 30
Dublin 28
Nanjing 28
Redondo Beach 27
Haiphong 26
Vienna 26
Baghdad 25
Chennai 25
Montreal 25
Council Bluffs 24
Guangzhou 24
Istanbul 24
Atlanta 23
Baku 23
Falkenstein 23
Warsaw 23
Amsterdam 22
Salt Lake City 22
Amman 21
Luanda 21
Managua 21
Montevideo 21
Stockholm 21
Ulan Bator 21
Addis Ababa 20
Conakry 20
Da Nang 20
Dakar 20
Mumbai 20
Andorra la Vella 19
Lahore 19
Tainan City 19
Yerevan 19
Ankara 18
Denver 18
Jeddah 18
Toronto 18
Kampala 17
Phoenix 17
Riga 17
Tripoli 17
Brooklyn 16
Libreville 16
Vientiane 16
Bridgetown 15
Johannesburg 15
Nairobi 15
Nouakchott 15
Paris 15
Riyadh 15
San José 15
Abu Dhabi 14
Dushanbe 14
Florence 14
Phnom Penh 14
Praia 14
Totale 8.534
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Nome #
Numerical and Experimental Investigation of Hybrid Rocket Motors Transient Behavior 577
Design and In-orbit Demonstration of REGULUS, an Iodine electric propulsion system 324
The "Vortex Reloaded" project: numerical investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 294
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) 286
Modeling and CFD Simulation of Regression Rate in Hybrid Rocket Motors 267
Investigation of different strategies for access to space of small satellites on a defined LEO orbit 265
CFD Simulation of a Hybrid Rocket Motor with Liquid Injection 258
Numerical Modeling of Paraffin-Based Fuels Behavior 255
Testing of a Long-Burning-Time Paraffin-Based Hybrid Rocket Motor 250
Design and testing of a hydrogen peroxide bipropellant thruster 248
Update on green chemical propulsion activities and achievements by the University of Padua and its spin-off T4I 245
Scaling Parameters of Swirling Oxidizer Injection in Hybrid Rocket Motors 244
Numerical Model to Analyze Transient Behavior and Instabilities on Hybrid Rocket Motors 244
Real-Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor 239
Design and Testing of a 3D Printed 10 N Hydrogen Peroxide Monopropellant Thruster 238
SPONGE: a Sounding Rocket Experiment for PMDs 236
Development of a Flow Control Valve for a Throttleable Hybrid Rocket Motor and Throttling Fire Tests 225
Regression Rate Design Tailoring Through Vortex Injection in Hybrid Rocket Motors 224
Investigation of Effect of Diaphragms on the Efficiency of Hybrid Rockets 222
Numerical and Experimental Investigation on Vortex Injection in Hybrid Rocket Motors 213
A numerical model to analyze the transient behavior and instabilities on hybrid rocket motors 211
Development and testing of an engineering model of a hydrogen peroxide based 1N propulsion unit 210
Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection - Part 2 208
REGULUS: Know-How Acquired on Iodine Propellant 208
Numerical analyses of thermal protection design in hybrid rocket motors 208
The SPONGE rexus project: Overview of a sounding rocket experiment for PMDs 206
Development and Testing of a Long Burning Time Lab-scale Paraffin-Based Hybrid Rocket Motor 205
REGULUS: Iodine Fed Plasma Propulsion System for Small Satellites 205
REGULUS: INTEGRATION AND TESTING OF AN IODINE ELECTRIC PROPULSION SYSTEM 205
Numerical Investigation of Hybrid Motors for the EU FP7 SPARTAN Program 200
A Simplified Thermal Analysis Model for Regeneratively Cooled Rocket Engine Thrust Chambers and Its Calibration with Experimental Data 197
Status and Achievements of the Hydrogen Peroxide Chemical Propulsion Research at Padua University 197
Numerical and Experimental Investigation of Unidirectional Vortex Injection in Hybrid Rocket Engines 196
Numerical Simulation of an Isochoric Combustion Chamber for Hybrid Rocket Propulsion 192
Design and Testing of a 3D Printed Regenerative Cooled Nozzle for a Hydrogen Peroxide based Bi-Propellant Thruster 190
CFD Simulations of Self-Pressurized Nitrous Oxide Hybrid Rocket Motors 189
Computational Fluid Dynamics Simulation of Regression Rate in Hybrid Rockets 188
Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection 187
Impact of propulsion system characteristics on the potential for cost reduction of earth observation missions at very low altitudes 187
Numerical Investigation of Hybrid Rocket Combustion Chamber Transient Behavior 184
Explicit analytical equations for single port hybrid rocket combustion chamber sizing 181
Integrated approach for hybrid rocket technology development 180
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 174
Experimental Investigation of a H2O2 Hybrid Rocket with Different Swirl Injections and Fuels 170
CONCEPTUAL DESIGN OF THE ELECTRIC PUMPS FOR THE HIGH-PERFORMANCE ENGINE OF A EUROPEAN LUNAR LANDER 169
Development of the Propulsion System for a Moon Drone Vehicle Demonstrator 169
Comparison between Different Re-Entry Technologies for Debris Mitigation in LEO 167
Computational fluid dynamics simulation of hybrid rockets of different scales 164
Development of a Cavitating Pintle for a Throttleable Hybrid Rocket Motor 162
Numerical and Experimental Activities in Support of the Development of Hybrid Rocket Engine for Soft-Landing Applications 160
Analysis of Fluid-dynamic Systems to Increase Combustion Efficiency in Hybrid Rockets 159
Explicit Analytical Equations for Single Port Hybrid Rocket Combustion Chamber Sizing 157
Real-Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor 155
Numerical simulation of hybrid rockets liquid injection and comparison with experiments 153
Numerical Model to Analyse Nozzle Termochemical Erosion 147
CFD Simulation of Regression Rate in Hybrid Rockets 145
Numerical and Experimental Activities in Support of the Development of Hybrid-Rocket Engine for softlanding applications 144
Integrated approach for hybrid rocket technology development 144
Testing and CFD simulation of diaphragm hybrid rocket motors 143
Testing and CFD Simulation of Diaphragm Hybrid Rocket Motors 142
Review of Alternative Sustainable Fuels for Hybrid Rocket Propulsion 139
Optimal use of electric propulsion for drag compensation in very low earth orbit on satellites with deployable solar panels 139
Numerical Simulations of an H2O2 Vortex Hybrid Rocket Motor 138
Numerical Investigation of Pressure-Fed Solutions for Paraffin-Based Hybrid Rocket Motors 138
Magnetic Enhanced Plasma Propulsion System for small-satellites IOD development 135
C/C-SiC Nozzle for a Long Burn-Time Hybrid Rocket: Design and Optimization, Manufacturing and Testing 134
Investigation of different strategies for access to space of small satellites on a defined LEO orbit 132
Preliminary Design of the European Advanced Reusable Satellite EARS 132
Numerical Investigation of the Effect of a Diaphragm on the Performance of a Hybrid Rocket Motor 130
Numerical Simulations of an Isochoric Hybrid Rocket Combustion Chamber and Comparison with Tests 130
Numerical optimization of hybrid sounding rockets through coupled motor-trajectory simulation 127
Numerical Simulations of a Paraffin-Hydrogen Peroxide Hybrid Rocket with Swirl Injection 126
Electric propulsion technology for low earth mission of micro/nano-satellites 126
Preliminary Design of the Propulsion Subsystem for the European Advanced Reusable Satellite (EARS) 125
Variations and Control of Thrust and Mixture Ratio in Hybrid Rocket Motors 122
Investigation of the influence of gas phase molecular mass variations on hybrid rocket regression rate 120
Variations and Control of Thrust and Mixture Ratio in Hybrid Rocket Motors 117
CFD Simulation in Support of SPARTAN Research Program 116
Hybrid rocket residuals - An overlooked topic 110
Testing of a Small HTP Monopropellant Thruster for Space Applications 101
Hybrid Rocket Motor Regression Rate Prediction trough CFD Simulations 96
Impact of propulsion system characteristics on the potential for cost reduction of earth observation missions at very low altitudes 94
OPTIMAL USE OF ELECTRIC PROPULSION FOR DRAG COMPENSATION IN VERY LOW EARTH ORBIT ON SATELLITES WITH DEPLOYABLE SOLAR PANELS 92
Ascent Trajectory Optimisation for Hybrid Propulsion Micro Launcher 87
Development and Test of an Innovative Hybrid Rocket Combustion Chamber 85
Totale 15.680
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Categoria #
all - tutte 43.331
article - articoli 12.955
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 56.286
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022819 17 97 58 23 76 35 20 77 78 48 91 199
2022/2023826 126 76 19 87 144 110 8 54 86 34 62 20
2023/2024652 25 62 28 75 52 92 37 71 29 50 67 64
2024/20252.339 18 141 102 124 245 122 104 238 220 73 377 575
2025/20268.397 348 568 1.077 1.405 963 334 910 936 753 478 387 238
2026/2027298 298 0 0 0 0 0 0 0 0 0 0 0
Totale 15.680