PASTRONE, Dario Giuseppe
 Distribuzione geografica
Continente #
NA - Nord America 15.261
EU - Europa 14.195
AS - Asia 8.318
SA - Sud America 666
AF - Africa 108
OC - Oceania 17
Continente sconosciuto - Info sul continente non disponibili 11
Totale 38.576
Nazione #
US - Stati Uniti d'America 15.144
IT - Italia 4.996
SG - Singapore 2.334
DE - Germania 2.134
GB - Regno Unito 1.938
CN - Cina 1.906
VN - Vietnam 1.794
FR - Francia 1.512
RU - Federazione Russa 1.077
UA - Ucraina 793
BR - Brasile 538
KR - Corea 534
HK - Hong Kong 391
TR - Turchia 366
NL - Olanda 351
IE - Irlanda 324
IN - India 297
SE - Svezia 206
CH - Svizzera 180
FI - Finlandia 155
JP - Giappone 135
BE - Belgio 125
CA - Canada 76
JO - Giordania 70
ES - Italia 65
TH - Thailandia 59
ID - Indonesia 53
IR - Iran 53
PH - Filippine 52
BD - Bangladesh 48
IQ - Iraq 47
AT - Austria 46
TW - Taiwan 43
MY - Malesia 40
PL - Polonia 38
AR - Argentina 37
BG - Bulgaria 33
EU - Europa 30
PT - Portogallo 30
AE - Emirati Arabi Uniti 25
IL - Israele 24
PK - Pakistan 24
MX - Messico 23
ZA - Sudafrica 23
RO - Romania 22
CO - Colombia 17
DZ - Algeria 15
AP - ???statistics.table.value.countryCode.AP??? 14
KZ - Kazakistan 14
SA - Arabia Saudita 14
VE - Venezuela 14
CL - Cile 13
EG - Egitto 13
PY - Paraguay 13
AU - Australia 12
EC - Ecuador 12
GR - Grecia 11
MA - Marocco 10
PE - Perù 10
BY - Bielorussia 9
ET - Etiopia 9
UZ - Uzbekistan 9
BO - Bolivia 8
CI - Costa d'Avorio 8
TN - Tunisia 8
CZ - Repubblica Ceca 7
LU - Lussemburgo 7
LV - Lettonia 7
KE - Kenya 6
LB - Libano 6
LT - Lituania 6
NG - Nigeria 6
NO - Norvegia 6
NP - Nepal 6
SN - Senegal 6
AL - Albania 5
HN - Honduras 5
HR - Croazia 5
OM - Oman 5
EE - Estonia 4
HU - Ungheria 4
IS - Islanda 4
NZ - Nuova Zelanda 4
UY - Uruguay 4
BA - Bosnia-Erzegovina 3
DK - Danimarca 3
SK - Slovacchia (Repubblica Slovacca) 3
SY - Repubblica araba siriana 3
TT - Trinidad e Tobago 3
AZ - Azerbaigian 2
BH - Bahrain 2
GA - Gabon 2
GP - Guadalupe 2
GT - Guatemala 2
JM - Giamaica 2
MD - Moldavia 2
PS - Palestinian Territory 2
RS - Serbia 2
TJ - Tagikistan 2
AO - Angola 1
Totale 38.563
Città #
Ashburn 3.453
Southend 1.648
Singapore 1.342
Seattle 1.224
Turin 1.196
Des Moines 1.099
Fairfield 950
San Jose 910
Chandler 552
Woodbridge 507
Ho Chi Minh City 472
Princeton 447
Beijing 430
Hanoi 421
Houston 417
Jacksonville 388
Santa Clara 345
Wilmington 343
Milan 330
Dublin 318
Ann Arbor 307
Cambridge 304
Hong Kong 304
San Ramon 274
Berlin 273
Seoul 262
Torino 255
Chicago 243
Dallas 230
Rome 226
Izmir 225
Boardman 200
Hefei 200
Zhengzhou 185
Los Angeles 168
Bern 164
Shanghai 158
Frankfurt 157
Lauterbourg 141
Helsinki 134
Moscow 129
San Donato Milanese 123
Council Bluffs 120
Brussels 116
Bologna 113
Herkenbosch 104
Baltimore 97
San Mauro Torinese 95
Pennsylvania Furnace 94
Zaporozhye 90
Overberg 83
Buffalo 81
New York 81
Da Nang 80
Haiphong 77
Denver 71
Hangzhou 63
Monopoli 62
Saint Petersburg 59
Padua 58
Amsterdam 53
Frankfurt am Main 50
Naples 49
Redwood City 48
Istanbul 46
Tokyo 45
Guangzhou 43
San Diego 42
Mountain View 39
São Paulo 38
Toronto 38
Genoa 37
Dearborn 34
Nichelino 33
Atlanta 32
Savigliano 32
The Dalles 32
Malatya 31
Rotterdam 31
Zogno 31
Hải Dương 30
Paris 29
San Francisco 28
Vienna 28
Chennai 27
Sofia 27
Warsaw 27
Ankara 26
Jakarta 26
Brooklyn 25
Munich 25
Bangkok 24
Redmond 23
Shenzhen 23
Verona 23
Cuneo 21
Bari 20
Norwalk 20
Pisa 20
Yubileyny 20
Totale 24.274
Nome #
Chemical Rocket Propulsion 512
Approaches to Low Fuel Regression Rate in Hybrid Rocket Engines 509
Combustion Instability Involving Vortex Shedding in Hybrid Rocket Motors 452
Performance of a small-scale turbojet engine fed with traditional and alternative fuels 429
Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper Stage 420
Active Debris Removal Missions with Multiple Targets 417
Design Trade-offs for Hybrid Rocket Motors 374
An Italian network to improve hybrid rocket performance: Strategy and results 373
Solid Rocket Propellant Photo-Polymerization with an In-House LED-UV Prototype 356
Comparative specific energy consumption between air transport and high-speed rail transport: A practical assessment 355
Risposta dinamica di presa d'aria supersonica a disturbi generati a monte e a valle dell'onda d'urto retta 353
Oxidizer Control and Optimal Design of Hybrid Rockets for Small Satellites 349
Comparison of Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper-Stage 339
Il problema di Goddard 337
Optimal Low-Thrust Escape Trajectories Using Gravity Assist 333
Analysis of Air-Turborocket Performance 332
Optimization Procedure for Preliminary Design of Opposition-Class Mars Missions 326
IMPACT OF AN OPTIMIZED POWER TURBINE DISKS CAVITY ON GEARED OPEN ROTOR PERFORMANCE – A MULTIDISCIPLINARY APPROACH IN THE PRELIMINARY DESIGN 325
Dual-bell nozzle with fluidic control of transition for space launchers 325
Optimization of Open Rotor Engines for Civil Aircraft Using a Cooperative Evolutionary Method 324
Mixture-Ratio Control to Improve Hydrogen-Fuel Rocket Performance 323
Effects of Limitation of Nozzle Flow Separation on Launcher Performance 323
Optimal design of hybrid rocket motors for microgravity platform 322
Hybrid rocket upper stage optimization: effects of grain geometry 322
Optimal Low-Thrust Trajectories Using Flyby 320
Rheological and Mechanical Characterization of 3D Printable Solid Propellant Slurry 315
Acoustic Analysis of Hybrid Rocket Combustion Chambers 309
An Indirect Method for the Optimization of Finite-Thrust Non-Coplanar Rendezvous Maneuvers 307
Analysis of Acoustics and Vortex Shedding Interactions in Hybrid Rocket Motors 301
Optimization of Hybrid Propellant Mars Ascent Vehicle 298
Acoustic Analysis of Hybrid Rocket Combustion Chambers 297
Optimal Performance of a Dual-Fuel Single-Stage Rocket 296
Simple Strategy for Powered Swingby 294
Photo-polymerization for additive manufacturing of composite solid propellants 294
Wall Curvature Effects on External Burning in Supersonic Flow 291
Numerical Analysis of Grain Burnback in Solid Propellants 291
Indirect Optimization Method for Round-Trip Mars Trajectories 290
Effects of limitation of nozzle flow separation on launcher performance 290
An Improved Acoustic Analysis of a Subscale Rocket Motor 289
Optimal Aeroassisted GEO-to-LEO Transfer by an Indirect Method 283
Optimization of an Advanced Open Rotor Engine for Civil Transport 281
Indirect Optimization Method for Impulsive Transfers 280
Modeling Combustion Instability in Aluminized Hybrid Propellants 278
A Straightforward Approach for Robust Design of Hybrid Rocket Engine Upper Stage 277
Optimization of Hybrid Upper-Stage Motor with Coupled Evolutionary/Indirect Procedure 277
Analysis of a Thermally Actuated Vuilleumier Refrigerator 275
Numerical Analysis of Grain Burnback in Solid Propellants 272
Mission opportunities for human exploration of Mars 272
Integrated Design of Hybrid Rocket Upper Stage and Launcher Trajectory 271
Optimal Design of Hybrid Rocket Motors for Launchers Upper Stages 270
Multiphysics Modeling for Combustion Instability in Paraffin-Fueled Hybrid Rocket Engines 267
Analysis of Conical Detonation Waves 263
Optimal Robust Design of Hybrid Rocket Engines 263
N2O-Cooled Aerospike for a Hybrid Rocket Motor: Nitrous Oxide Characterization and Additive Manufacturing 260
GTOC5: Results from the Politecnico di Torino and Università di Roma Sapienza 259
Experimental investigation of the effects of different internal surface features on additive-manufactured resonant igniters performance 258
Comparison of Robust Design Approaches for Hybrid Rocket Engines 258
Multi physics modelling for a hybrid rocket engine with liquefying fuel: a sensitivity analysis on combustion instability 254
Optimization of rocket ascent trajectories using an indirect procedure 253
Mixture-Ratio Control to Improve LOX/LH2 Rocket Performance 252
Blockage Corrections at High Angles of Attack in a Wind Tunnel 252
Advancements in Photocurable Solid Propellantsfor Additive Manufacturing 251
Optimization of DeltaV-Earth-Gravity-Assist Trajectories 250
Optimal Performance of a Tripropellant Single-Stage Rocket 249
Optimal Finite-Thrust Spacecraft Trajectories: an Indirect Approach 249
Modeling of Saturated and Superheated N2O Heat Transfer Rates, with Experimental Verification 249
Optimization of DV-Earth-Gravity-Assist Trajectories 249
Traiettorie ottimali di ascesa in orbita 248
Simple Strategy for Powered Swingby 248
Design Optimization of a Mg/CO2 Hybrid Rocket Engine for Mars Ascent Vehicles 247
Optimal Design of Hybrid Rocket Motors for Launchers Upper Stages 245
Hybrid rocket engine design optimization at politecnico di torino: A review 245
Analysis of a Stator-Rotor-Stator Spinning Disk Reactor in Single-Phase and Two-Phase Boiling Conditions Using a Thermo-Fluid Flow Network and CFD 244
A Parametric Analysis of Hybrid Rocket Motors for Sounding Rockets 243
Optimal Design and Control of Hybrid Rockets for Access to Space 243
Optimal Three-Dimensional Trajectories for Manned Mars Missions 243
Optimization of Hybrid Sounding Rockets for Hypersonic Testing 243
An Analysis of Air-Turborocket Performance 242
Numerical Tracking of the Solid-Gas Interface in Rocket Motors 242
Optimal Design of Hybrid Rockets for Small Satellites 241
Optimization of Civil Turbofan with Evolutionary Algorithms 241
An Indirect Method for Fixed-Time Finite-Thrust Optimal Orbit Transfer 241
Evaluation of UV-Curable Solid Rocket Propellants’ Properties for Advanced 3D Printing Technologies 240
Multi-Objective Optimization of Rocket-Based Combined-Cycle Engine Performance Using a Hybrid Evolutionary Algorithm 238
External burning on curved surfaces in supersonic flow - Problems and limitations 238
Optimal Design of Hybrid Rocket Small Satellite Launchers: Ground Versus Airborne Launch 238
Oxidizer Control and Optimal Design of Hybrid Rockets for Small Satellites 237
Optimal performance of a dual-fuel single-stage rocket 236
AN ITALIAN NETWORK TO IMPROVE HYBRID ROCKET PERFORMANCE: THE STRATEGY, THE PROGRAM, THE RESULTS 236
An Air-Turborocket Exergy Analysis 235
Viability of an Electrically Driven Pump-Fed Hybrid Rocket for Small Launcher Upper Stages 235
Optimal Orbit Transfer Using a Canonical Transformation and an Indirect Method 235
Deterministic and Robust Optimization of Hybrid Rocket Engines for Small Satellite Launchers 233
Optimization of a Hybrid Rocket Upper Stage with Electric Pump Feed System 232
Assessment of Mission Capabilities of a Reusable Heavy-lift Launch Vehicle Concept with Aerospike Engine 231
Pressure-Measurement Based Estimation of Fuel Regression Rate in Hybrid Rockets 231
Multi-objective Optimization of Electric Pumps for Hybrid Rocket Engines 230
Integrated Design-Trajectory Optimization for Hybrid Rocket Motors 230
Evolutionary Algorithm Based Approach for RBCC Engines Optimization 228
Emission-Driven Hybrid Rocket Engine Optimization for Small Launchers 227
Totale 28.550
Categoria #
all - tutte 103.153
article - articoli 35.897
book - libri 0
conference - conferenze 56.730
curatela - curatele 0
other - altro 691
patent - brevetti 524
selected - selezionate 0
volume - volumi 9.311
Totale 206.306


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021257 0 0 0 0 0 0 0 0 0 0 134 123
2021/20221.706 69 79 197 50 45 90 189 77 110 121 262 417
2022/20233.574 222 393 66 168 210 360 1.272 179 300 57 120 227
2023/20241.422 60 102 58 94 124 194 117 245 47 119 125 137
2024/20253.625 48 444 166 342 363 205 224 264 451 222 379 517
2025/20269.389 520 510 678 774 477 588 1.504 796 2.245 1.084 213 0
Totale 38.920