BARATO, FRANCESCO
 Distribuzione geografica
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Continente #
NA - Nord America 3.404
EU - Europa 687
AS - Asia 291
OC - Oceania 9
AF - Africa 3
SA - Sud America 2
Totale 4.396
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Nazione #
US - Stati Uniti d'America 3.394
IT - Italia 345
CN - Cina 160
DE - Germania 86
FI - Finlandia 59
GB - Regno Unito 52
SE - Svezia 41
IN - India 37
TW - Taiwan 24
FR - Francia 21
JP - Giappone 19
IE - Irlanda 18
UA - Ucraina 17
NL - Olanda 15
CA - Canada 10
HK - Hong Kong 10
IR - Iran 9
BE - Belgio 8
TR - Turchia 8
AU - Australia 7
ES - Italia 7
KR - Corea 7
AE - Emirati Arabi Uniti 6
RO - Romania 6
SG - Singapore 6
LB - Libano 4
PL - Polonia 4
PT - Portogallo 4
EG - Egitto 3
CL - Cile 2
DK - Danimarca 2
NZ - Nuova Zelanda 2
LK - Sri Lanka 1
LU - Lussemburgo 1
NO - Norvegia 1
Totale 4.396
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Città #
Fairfield 604
Chandler 337
Ashburn 298
Woodbridge 288
Seattle 256
Wilmington 225
Houston 218
Cambridge 206
Ann Arbor 189
New York 72
Medford 70
Princeton 70
San Diego 61
Padova 59
Des Moines 57
Beijing 56
Roxbury 46
Boardman 35
Helsinki 32
Nanjing 28
Rome 26
Milan 23
Dublin 18
London 14
Jacksonville 12
Napoli 12
Tainan City 12
Nanchang 11
Turin 11
Hebei 10
Redwood City 9
Romano di Lombardia 9
Shenyang 8
Stigliano 8
Delft 7
Lazzate 7
Leeds 7
Abu Dhabi 6
Bologna 6
Cagliari 6
Guangzhou 6
Hong Kong 6
Istanbul 6
Nürnberg 6
Ogden 6
Paris 6
Taoyuan District 6
Tehran 6
Lappeenranta 5
Melbourne 5
Munich 5
Norwalk 5
Selvazzano Dentro 5
Thierhaupten 5
Brussels 4
Central 4
Changsha 4
Chennai 4
Jinan 4
La Calamine 4
Madrid 4
Naples 4
Santa Maria 4
Siddipet 4
Venice 4
Wuhan 4
Xi'an 4
Arroyo Grande 3
Bonndorf 3
Cairo 3
Calgary 3
Chengdu 3
Dallas 3
Hefei 3
Kunming 3
Lanzhou 3
Rijswijk 3
Sesto San Giovanni 3
Shanghai 3
Spinea 3
Taipei 3
Thrissur 3
Aachen 2
Alella 2
Amsterdam 2
Atlanta 2
Auckland 2
Aveiro 2
Bade District 2
Barlassina 2
Bengaluru 2
Brendola 2
Buk-gu 2
Burke 2
Busan 2
Copenhagen 2
Dulles 2
Edmonton 2
Florence 2
Grosseto 2
Totale 3.640
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Nome #
Numerical and Experimental Investigation of Hybrid Rocket Motors Transient Behavior 191
The "Vortex Reloaded" project: numerical investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 171
Scaling Parameters of Swirling Oxidizer Injection in Hybrid Rocket Motors 119
Design and Testing of a 3D Printed 10 N Hydrogen Peroxide Monopropellant Thruster 112
Real-Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor 110
Testing of a Long-Burning-Time Paraffin-Based Hybrid Rocket Motor 105
Regression Rate Design Tailoring Through Vortex Injection in Hybrid Rocket Motors 102
Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection - Part 2 100
Development of a Flow Control Valve for a Throttleable Hybrid Rocket Motor and Throttling Fire Tests 100
Design and In-orbit Demonstration of REGULUS, an Iodine electric propulsion system 99
Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection 97
Development and Testing of a Long Burning Time Lab-scale Paraffin-Based Hybrid Rocket Motor 97
Numerical and Experimental Investigation on Vortex Injection in Hybrid Rocket Motors 96
CFD Simulation of a Hybrid Rocket Motor with Liquid Injection 95
Investigation of Effect of Diaphragms on the Efficiency of Hybrid Rockets 91
Computational Fluid Dynamics Simulation of Regression Rate in Hybrid Rockets 88
A numerical model to analyze the transient behavior and instabilities on hybrid rocket motors 88
Numerical Modeling of Paraffin-Based Fuels Behavior 88
CFD Simulations of Self-Pressurized Nitrous Oxide Hybrid Rocket Motors 88
Numerical Model to Analyze Transient Behavior and Instabilities on Hybrid Rocket Motors 85
SPONGE: a Sounding Rocket Experiment for PMDs 84
Numerical Investigation of Hybrid Motors for the EU FP7 SPARTAN Program 84
Impact of propulsion system characteristics on the potential for cost reduction of earth observation missions at very low altitudes 80
Testing and CFD Simulation of Diaphragm Hybrid Rocket Motors 75
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) 75
Numerical Investigation of Hybrid Rocket Combustion Chamber Transient Behavior 73
The SPONGE rexus project: Overview of a sounding rocket experiment for PMDs 72
Integrated approach for hybrid rocket technology development 72
The "Vortex Reloaded" project: experimental investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 71
Explicit Analytical Equations for Single Port Hybrid Rocket Combustion Chamber Sizing 70
Testing and CFD simulation of diaphragm hybrid rocket motors 69
Numerical and Experimental Investigation of Unidirectional Vortex Injection in Hybrid Rocket Engines 69
Status and Achievements of the Hydrogen Peroxide Chemical Propulsion Research at Padua University 68
Numerical Simulation of an Isochoric Combustion Chamber for Hybrid Rocket Propulsion 63
Numerical analyses of thermal protection design in hybrid rocket motors 63
Computational fluid dynamics simulation of hybrid rockets of different scales 60
Explicit analytical equations for single port hybrid rocket combustion chamber sizing 57
Numerical simulation of hybrid rockets liquid injection and comparison with experiments 57
Design and testing of a hydrogen peroxide bipropellant thruster 57
REGULUS: Know-How Acquired on Iodine Propellant 56
REGULUS: INTEGRATION AND TESTING OF AN IODINE ELECTRIC PROPULSION SYSTEM 54
Numerical and Experimental Activities in Support of the Development of Hybrid Rocket Engine for Soft-Landing Applications 52
Integrated approach for hybrid rocket technology development 51
Development of a Cavitating Pintle for a Throttleable Hybrid Rocket Motor 43
Numerical Investigation of the Effect of a Diaphragm on the Performance of a Hybrid Rocket Motor 42
Analysis of Fluid-dynamic Systems to Increase Combustion Efficiency in Hybrid Rockets 42
REGULUS: Iodine Fed Plasma Propulsion System for Small Satellites 41
Electric propulsion technology for low earth mission of micro/nano-satellites 40
Numerical Investigation of Pressure-Fed Solutions for Paraffin-Based Hybrid Rocket Motors 39
CFD Simulation in Support of SPARTAN Research Program 38
Variations and Control of Thrust and Mixture Ratio in Hybrid Rocket Motors 38
Numerical Simulations of an H2O2 Vortex Hybrid Rocket Motor 37
Numerical and Experimental Activities in Support of the Development of Hybrid-Rocket Engine for softlanding applications 37
C/C-SiC Nozzle for a Long Burn-Time Hybrid Rocket: Design and Optimization, Manufacturing and Testing 36
CFD Simulation of Regression Rate in Hybrid Rockets 35
Hybrid rocket residuals - An overlooked topic 34
Numerical Simulations of an Isochoric Hybrid Rocket Combustion Chamber and Comparison with Tests 32
Magnetic Enhanced Plasma Propulsion System for small-satellites IOD development 30
Design and Testing of a 3D Printed Regenerative Cooled Nozzle for a Hydrogen Peroxide based Bi-Propellant Thruster 30
Challenges of ablatively cooled hybrid rockets for satellites or upper stages 27
Variations and Control of Thrust and Mixture Ratio in Hybrid Rocket Motors 26
Numerical Model to Analyse Nozzle Termochemical Erosion 24
Development of the Propulsion System for a Moon Drone Vehicle Demonstrator 24
Real-Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor 21
A Simplified Thermal Analysis Model for Regeneratively Cooled Rocket Engine Thrust Chambers and Its Calibration with Experimental Data 19
Modeling and CFD Simulation of Regression Rate in Hybrid Rocket Motors 18
OPTIMAL USE OF ELECTRIC PROPULSION FOR DRAG COMPENSATION IN VERY LOW EARTH ORBIT ON SATELLITES WITH DEPLOYABLE SOLAR PANELS 18
Development and Test of an Innovative Hybrid Rocket Combustion Chamber 16
Numerical optimization of hybrid sounding rockets through coupled motor-trajectory simulation 14
Ascent Trajectory Optimisation for Hybrid Propulsion Micro Launcher 12
Hybrid Rocket Motor Regression Rate Prediction trough CFD Simulations 10
Impact of propulsion system characteristics on the potential for cost reduction of earth observation missions at very low altitudes 8
Comparison between Different Re-Entry Technologies for Debris Mitigation in LEO 6
Review of Alternative Sustainable Fuels for Hybrid Rocket Propulsion 4
Optimal use of electric propulsion for drag compensation in very low earth orbit on satellites with deployable solar panels 4
CONCEPTUAL DESIGN OF THE ELECTRIC PUMPS FOR THE HIGH-PERFORMANCE ENGINE OF A EUROPEAN LUNAR LANDER 2
Totale 4.501
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Categoria #
all - tutte 15.567
article - articoli 4.977
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 20.544
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019197 0 0 0 0 0 0 0 0 0 48 87 62
2019/2020865 76 14 39 69 103 61 89 105 101 78 121 9
2020/20211.073 32 18 24 146 376 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
2023/2024507 25 62 28 75 52 92 37 71 29 36 0 0
Totale 4.501