BARATO, FRANCESCO
 Distribuzione geografica
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Continente #
NA - Nord America 4.939
AS - Asia 2.907
EU - Europa 2.145
AF - Africa 664
SA - Sud America 510
OC - Oceania 74
Continente sconosciuto - Info sul continente non disponibili 21
Totale 11.260
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Nazione #
US - Stati Uniti d'America 4.618
SG - Singapore 979
IT - Italia 633
CN - Cina 487
HK - Hong Kong 353
BR - Brasile 299
DE - Germania 233
VN - Vietnam 227
NL - Olanda 136
FI - Finlandia 126
GB - Regno Unito 115
IN - India 103
FR - Francia 93
PL - Polonia 85
SE - Svezia 79
TR - Turchia 68
RU - Federazione Russa 64
CI - Costa d'Avorio 63
JP - Giappone 57
TW - Taiwan 56
CA - Canada 47
UA - Ucraina 45
AR - Argentina 43
ES - Italia 42
KR - Corea 39
BJ - Benin 37
IE - Irlanda 35
ID - Indonesia 34
MX - Messico 32
PK - Pakistan 32
AT - Austria 28
AE - Emirati Arabi Uniti 27
MA - Marocco 27
BE - Belgio 26
IL - Israele 25
IR - Iran 24
PY - Paraguay 24
AO - Angola 23
CO - Colombia 23
DZ - Algeria 23
CH - Svizzera 22
GN - Guinea 22
AU - Australia 21
AZ - Azerbaigian 21
CR - Costa Rica 21
KZ - Kazakistan 21
SA - Arabia Saudita 21
BF - Burkina Faso 20
BY - Bielorussia 20
CL - Cile 20
EC - Ecuador 20
IQ - Iraq 20
LB - Libano 20
LY - Libia 20
NO - Norvegia 20
NP - Nepal 20
SK - Slovacchia (Repubblica Slovacca) 20
UY - Uruguay 20
ZA - Sudafrica 20
AD - Andorra 19
CZ - Repubblica Ceca 19
DK - Danimarca 19
JM - Giamaica 19
MN - Mongolia 19
NI - Nicaragua 19
SN - Senegal 19
TH - Thailandia 19
AM - Armenia 18
BA - Bosnia-Erzegovina 18
BO - Bolivia 18
HR - Croazia 18
HU - Ungheria 18
IS - Islanda 18
JO - Giordania 18
LV - Lettonia 18
PT - Portogallo 18
RE - Reunion 18
RO - Romania 18
UG - Uganda 18
CV - Capo Verde 17
GA - Gabon 17
HN - Honduras 17
HT - Haiti 17
LA - Repubblica Popolare Democratica del Laos 17
MD - Moldavia 17
PH - Filippine 17
YT - Mayotte 17
BB - Barbados 16
KE - Kenya 16
MR - Mauritania 16
BD - Bangladesh 15
CG - Congo 15
CM - Camerun 15
GE - Georgia 15
GR - Grecia 15
KG - Kirghizistan 15
KH - Cambogia 15
PE - Perù 15
RS - Serbia 15
SI - Slovenia 15
Totale 10.601
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Città #
Fairfield 604
Singapore 474
Ashburn 456
Chandler 337
Hong Kong 331
Woodbridge 288
Seattle 259
Wilmington 231
Houston 222
Cambridge 206
Ann Arbor 189
Beijing 187
Santa Clara 178
Boardman 112
New York 106
Ho Chi Minh City 84
Los Angeles 82
Padova 81
Medford 70
Princeton 70
Rome 68
San Diego 61
Abidjan 60
Munich 60
Chicago 58
Des Moines 57
Helsinki 53
Bytom 49
Milan 49
Roxbury 46
Hanoi 43
Cotonou 36
Turku 36
São Paulo 32
Buffalo 28
Nanjing 28
Dublin 27
London 27
Redondo Beach 27
Turin 26
Falkenstein 23
Vienna 23
Salt Lake City 22
Conakry 20
Dallas 20
Luanda 20
Stockholm 20
Warsaw 20
Andorra la Vella 19
Baku 19
Dakar 19
Managua 19
Tainan City 19
Ulan Bator 19
Amman 18
Tokyo 18
Kampala 17
Montreal 17
Tripoli 17
Frankfurt am Main 16
Libreville 16
Montevideo 16
Vientiane 16
Yerevan 16
Bridgetown 15
Denver 15
Istanbul 15
Naples 15
Riga 15
Ankara 14
Dushanbe 14
Nouakchott 14
Phnom Penh 14
Praia 14
Abu Dhabi 13
Brussels 13
Chennai 13
Minsk 13
Noumea 13
Reykjavik 13
Tashkent 13
Zagreb 13
Atlanta 12
Bamako 12
Bishkek 12
Delft 12
Hefei 12
Jacksonville 12
Lahore 12
Mumbai 12
Napoli 12
Phoenix 12
Tbilisi 12
Accra 11
Addis Ababa 11
Amsterdam 11
Antananarivo 11
Bologna 11
Brooklyn 11
Chisinau 11
Totale 6.345
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Nome #
Numerical and Experimental Investigation of Hybrid Rocket Motors Transient Behavior 429
The "Vortex Reloaded" project: numerical investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 234
Design and In-orbit Demonstration of REGULUS, an Iodine electric propulsion system 230
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) 213
Investigation of different strategies for access to space of small satellites on a defined LEO orbit 208
Design and Testing of a 3D Printed 10 N Hydrogen Peroxide Monopropellant Thruster 200
Scaling Parameters of Swirling Oxidizer Injection in Hybrid Rocket Motors 199
Testing of a Long-Burning-Time Paraffin-Based Hybrid Rocket Motor 197
SPONGE: a Sounding Rocket Experiment for PMDs 193
Regression Rate Design Tailoring Through Vortex Injection in Hybrid Rocket Motors 183
Real-Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor 181
Modeling and CFD Simulation of Regression Rate in Hybrid Rocket Motors 178
Numerical and Experimental Investigation on Vortex Injection in Hybrid Rocket Motors 178
Numerical Modeling of Paraffin-Based Fuels Behavior 178
Investigation of Effect of Diaphragms on the Efficiency of Hybrid Rockets 176
CFD Simulation of a Hybrid Rocket Motor with Liquid Injection 175
Development of a Flow Control Valve for a Throttleable Hybrid Rocket Motor and Throttling Fire Tests 174
Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection - Part 2 172
The SPONGE rexus project: Overview of a sounding rocket experiment for PMDs 170
Development and Testing of a Long Burning Time Lab-scale Paraffin-Based Hybrid Rocket Motor 169
A numerical model to analyze the transient behavior and instabilities on hybrid rocket motors 165
Numerical Model to Analyze Transient Behavior and Instabilities on Hybrid Rocket Motors 164
Design and testing of a hydrogen peroxide bipropellant thruster 162
CFD Simulations of Self-Pressurized Nitrous Oxide Hybrid Rocket Motors 159
Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection 158
Computational Fluid Dynamics Simulation of Regression Rate in Hybrid Rockets 156
Numerical Investigation of Hybrid Motors for the EU FP7 SPARTAN Program 155
Numerical analyses of thermal protection design in hybrid rocket motors 155
Impact of propulsion system characteristics on the potential for cost reduction of earth observation missions at very low altitudes 154
Status and Achievements of the Hydrogen Peroxide Chemical Propulsion Research at Padua University 152
The "Vortex Reloaded" project: experimental investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 148
Integrated approach for hybrid rocket technology development 146
REGULUS: Know-How Acquired on Iodine Propellant 146
REGULUS: INTEGRATION AND TESTING OF AN IODINE ELECTRIC PROPULSION SYSTEM 144
Numerical Investigation of Hybrid Rocket Combustion Chamber Transient Behavior 141
Numerical Simulation of an Isochoric Combustion Chamber for Hybrid Rocket Propulsion 139
Numerical and Experimental Investigation of Unidirectional Vortex Injection in Hybrid Rocket Engines 139
Computational fluid dynamics simulation of hybrid rockets of different scales 134
Explicit Analytical Equations for Single Port Hybrid Rocket Combustion Chamber Sizing 132
Design and Testing of a 3D Printed Regenerative Cooled Nozzle for a Hydrogen Peroxide based Bi-Propellant Thruster 132
CONCEPTUAL DESIGN OF THE ELECTRIC PUMPS FOR THE HIGH-PERFORMANCE ENGINE OF A EUROPEAN LUNAR LANDER 129
Challenges of ablatively cooled hybrid rockets for satellites or upper stages 129
Explicit analytical equations for single port hybrid rocket combustion chamber sizing 127
REGULUS: Iodine Fed Plasma Propulsion System for Small Satellites 125
Numerical simulation of hybrid rockets liquid injection and comparison with experiments 123
A Simplified Thermal Analysis Model for Regeneratively Cooled Rocket Engine Thrust Chambers and Its Calibration with Experimental Data 121
Testing and CFD Simulation of Diaphragm Hybrid Rocket Motors 120
Numerical and Experimental Activities in Support of the Development of Hybrid Rocket Engine for Soft-Landing Applications 119
Analysis of Fluid-dynamic Systems to Increase Combustion Efficiency in Hybrid Rockets 116
Testing and CFD simulation of diaphragm hybrid rocket motors 115
Real-Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor 115
Integrated approach for hybrid rocket technology development 114
Development of a Cavitating Pintle for a Throttleable Hybrid Rocket Motor 112
Numerical Investigation of Pressure-Fed Solutions for Paraffin-Based Hybrid Rocket Motors 111
Numerical Simulations of an H2O2 Vortex Hybrid Rocket Motor 108
CFD Simulation of Regression Rate in Hybrid Rockets 108
Numerical and Experimental Activities in Support of the Development of Hybrid-Rocket Engine for softlanding applications 106
C/C-SiC Nozzle for a Long Burn-Time Hybrid Rocket: Design and Optimization, Manufacturing and Testing 105
Development and testing of an engineering model of a hydrogen peroxide based 1N propulsion unit 104
Electric propulsion technology for low earth mission of micro/nano-satellites 103
Magnetic Enhanced Plasma Propulsion System for small-satellites IOD development 97
Development of the Propulsion System for a Moon Drone Vehicle Demonstrator 97
Numerical Investigation of the Effect of a Diaphragm on the Performance of a Hybrid Rocket Motor 96
Update on green chemical propulsion activities and achievements by the University of Padua and its spin-off T4I 94
Comparison between Different Re-Entry Technologies for Debris Mitigation in LEO 91
Review of Alternative Sustainable Fuels for Hybrid Rocket Propulsion 90
Variations and Control of Thrust and Mixture Ratio in Hybrid Rocket Motors 90
Experimental Investigation of a H2O2 Hybrid Rocket with Different Swirl Injections and Fuels 89
CFD Simulation in Support of SPARTAN Research Program 89
Variations and Control of Thrust and Mixture Ratio in Hybrid Rocket Motors 85
Numerical Simulations of an Isochoric Hybrid Rocket Combustion Chamber and Comparison with Tests 84
Numerical optimization of hybrid sounding rockets through coupled motor-trajectory simulation 82
Numerical Model to Analyse Nozzle Termochemical Erosion 81
Hybrid rocket residuals - An overlooked topic 79
Investigation of different strategies for access to space of small satellites on a defined LEO orbit 77
Optimal use of electric propulsion for drag compensation in very low earth orbit on satellites with deployable solar panels 77
Investigation of the influence of gas phase molecular mass variations on hybrid rocket regression rate 77
Preliminary Design of the European Advanced Reusable Satellite EARS 75
Numerical Simulations of a Paraffin-Hydrogen Peroxide Hybrid Rocket with Swirl Injection 73
OPTIMAL USE OF ELECTRIC PROPULSION FOR DRAG COMPENSATION IN VERY LOW EARTH ORBIT ON SATELLITES WITH DEPLOYABLE SOLAR PANELS 68
Development and Test of an Innovative Hybrid Rocket Combustion Chamber 65
Preliminary Design of the Propulsion Subsystem for the European Advanced Reusable Satellite (EARS) 63
Hybrid Rocket Motor Regression Rate Prediction trough CFD Simulations 63
Impact of propulsion system characteristics on the potential for cost reduction of earth observation missions at very low altitudes 63
Ascent Trajectory Optimisation for Hybrid Propulsion Micro Launcher 60
Testing of a Small HTP Monopropellant Thruster for Space Applications 58
Totale 11.391
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Categoria #
all - tutte 34.116
article - articoli 10.245
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 44.361
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021477 0 0 0 0 0 34 16 92 98 53 100 84
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
2025/20264.406 348 568 1.077 1.405 963 45 0 0 0 0 0 0
Totale 11.391