CINECA IRIS Institutional Research Information System

PASINI, ANGELO
 Distribuzione geografica
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Continente #
NA - Nord America 11.608
AS - Asia 6.440
EU - Europa 6.171
SA - Sud America 811
Continente sconosciuto - Info sul continente non disponibili 422
AF - Africa 164
OC - Oceania 112
Totale 25.728
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Nazione #
US - Stati Uniti d'America 11.182
IT - Italia 2.576
SG - Singapore 1.683
CN - Cina 1.668
HK - Hong Kong 988
SE - Svezia 757
BR - Brasile 664
DE - Germania 557
VN - Vietnam 514
GB - Regno Unito 418
FR - Francia 397
IN - India 316
TR - Turchia 306
CA - Canada 294
BG - Bulgaria 288
JP - Giappone 224
FI - Finlandia 175
KR - Corea 169
RU - Federazione Russa 169
ES - Italia 151
NL - Olanda 150
UA - Ucraina 147
AU - Australia 75
CH - Svizzera 75
BD - Bangladesh 64
MX - Messico 62
IR - Iran 57
AT - Austria 54
PL - Polonia 53
TH - Thailandia 47
AR - Argentina 46
TW - Taiwan 46
PH - Filippine 44
PK - Pakistan 42
BE - Belgio 41
MA - Marocco 41
IQ - Iraq 38
PT - Portogallo 38
NZ - Nuova Zelanda 36
SA - Arabia Saudita 36
ZA - Sudafrica 36
ID - Indonesia 35
KE - Kenya 26
IE - Irlanda 25
UZ - Uzbekistan 23
VE - Venezuela 21
AE - Emirati Arabi Uniti 20
CO - Colombia 20
MY - Malesia 20
CL - Cile 18
CI - Costa d'Avorio 14
LT - Lituania 14
EC - Ecuador 13
EG - Egitto 13
GR - Grecia 13
JM - Giamaica 13
PE - Perù 13
DZ - Algeria 12
AZ - Azerbaigian 11
IL - Israele 11
RO - Romania 11
CR - Costa Rica 10
NP - Nepal 10
JO - Giordania 9
TN - Tunisia 9
CZ - Repubblica Ceca 8
PS - Palestinian Territory 8
DO - Repubblica Dominicana 7
HU - Ungheria 7
NI - Nicaragua 7
NO - Norvegia 7
PY - Paraguay 7
EE - Estonia 6
HN - Honduras 6
KZ - Kazakistan 6
OM - Oman 6
UY - Uruguay 6
GE - Georgia 5
HR - Croazia 5
LU - Lussemburgo 5
PA - Panama 5
TT - Trinidad e Tobago 5
BH - Bahrain 4
CY - Cipro 4
DK - Danimarca 4
LK - Sri Lanka 4
MO - Macao, regione amministrativa speciale della Cina 4
AL - Albania 3
BA - Bosnia-Erzegovina 3
KW - Kuwait 3
LB - Libano 3
MK - Macedonia 3
NG - Nigeria 3
PR - Porto Rico 3
SK - Slovacchia (Repubblica Slovacca) 3
SV - El Salvador 3
BJ - Benin 2
BO - Bolivia 2
CG - Congo 2
ET - Etiopia 2
Totale 25.269
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Città #
Ashburn 1.088
Woodbridge 1.015
Dallas 960
Singapore 923
Hong Kong 916
San Jose 781
Fairfield 613
Houston 587
Santa Clara 586
Shanghai 567
Ann Arbor 559
Milan 536
Chandler 383
Pisa 322
Beijing 297
Sofia 288
Seattle 258
New York 248
Wilmington 248
Council Bluffs 235
Los Angeles 231
Cambridge 212
Rome 207
Boardman 171
Ottawa 160
Jacksonville 158
Serra 157
Florence 148
Ho Chi Minh City 135
Izmir 134
Princeton 122
Lawrence 116
Lauterbourg 115
Frankfurt am Main 111
Tokyo 109
Hefei 105
Hanoi 101
Nanjing 95
Buffalo 74
Istanbul 70
Helsinki 67
Munich 62
Dearborn 59
Seoul 58
Paris 56
São Paulo 56
Medford 54
Columbus 48
Bern 46
Ankara 44
Bangkok 44
Southampton 43
Des Moines 42
Kent 42
London 41
Redondo Beach 41
Düsseldorf 38
Orem 38
The Dalles 38
Toronto 36
Turin 36
Chicago 35
Dong Ket 34
Mumbai 34
Boulder 33
Lucca 33
San Diego 32
Turku 32
Madrid 31
Bengaluru 30
Delft 30
Jüchen 30
Chennai 29
Nanchang 29
Hyderabad 28
Melbourne 28
Phoenix 28
Berlin 27
Ogden 27
Warsaw 27
Amsterdam 26
Casablanca 26
Montreal 26
Naples 26
Pune 26
Shenyang 26
Barcelona 25
Belo Horizonte 25
Nairobi 25
Vienna 25
Changsha 24
Glasgow 24
Manchester 23
Redwood City 23
Brussels 22
West Lafayette 22
Bologna 21
Guangzhou 21
Livorno 21
City of London 20
Totale 16.184
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Nome #
Eco-design of future reusable launchers: insight into their life-cycle and atmospheric impact 1.092
Design of a Modular 1U Propellant Tank for CubeSats HTP Monopropellant Propulsion System 536
Assessment of Propulsion System Architectures for Green Propellants-based Orbital Stages 532
Three-dimensional deployment of cable nets for active removal of space debris 409
Deployable cable nets for active removal of derelict rocket bodies 407
Development of the EXCITE IOD/IOV mission 350
LUNANOVA KICK STAGE STUDY: AN OVERVIEW OF THE SYSTEM PROPULSION TRADEOFFS 322
Development of a High Power, Magnetically Shielded, Dual Channel Hall Thruster in The Framework of the TANDEM Project 307
TANDEM: a High Power, Magnetically Shielded Hall Thruster with a Nested Configuration 304
Development of High Speed Hybrid Bearings for Reusable Pump-Fed Liquid Rocket Engines 296
Nuclear Thermal Propulsion for Earth Orbit and Interplanetary Missions: Challenges and Issues. 292
CubeSat Green Propellants AM Tanks: Efficient Designs, Propellant Management, And Chemical Compatibility 282
On the Preliminary Design and Noncavitating Performance of Tapered Axial Inducers 269
Cavitating Pump Rotordynamic Test Facility at ALTA S.p.A.: Upgraded Capabilities of a Unique Test Rig 243
Turbopump Design: Comparison of Numerical Simulations to an Already Validated Reduced-Order Model 242
Experimental Characterization of a 5 N Hydrogen Peroxide Monopropellant Thruster Prototype 234
Design of an Affordable Hydrogen Peroxide Propulsion System for CubeSats 234
Use of Pt/CexZr1-xAl2O3 as Advanced Catalyst for Hydrogen Peroxide Thrusters 230
Performance Modeling and Analysis of H2O2 Catalytic Pellet Reactors 228
Testing and Characterization of a Hydrogen Peroxide Monopropellant Thruster 227
Cavitation and Turbopump Hydrodynamics Research at Alta S.P.A. and Pisa University 227
Rotordynamic Forces on a Four Bladed Inducer 226
Performance of Different Catalysts Supported on Alumina Spheres for Hydrogen Peroxide Decomposition 225
Cavitation and Flow Instabilities in a 3- Bladed Axial Inducer Designed by Means of a Reduced Order Analytical Model 225
Development of Hydrogen Peroxide Rockets at Alta S.p.A.: the Past, the Present and the Future 223
A Reduced Order Model for Optimal Centrifugal Pump Design 220
Theoretical Optimization of Splitter Blade Geometry in High-Efficiency Centrifugal Turbopumps 220
Platinum catalysts development for 98% hydrogen peroxide decomposition in pulsed monopropellant thrusters 218
Continuous Spectrum of the Rotordynamic Forces on a Four Bladed Inducer 212
Comparative Characterization of Advanced Catalytic Beds for Hydrogen Peroxide Thrusters 206
Maximum Likelihood Identification of Cavitation Instabilities in Axial Inducers 206
Inducer and centrifugal pump contributions to the rotordynamic fluid forces acting on a space turbopump 203
A Reduced Order Model for Preliminary Design and Performance Prediction of Tapered Inducers: Comparison with Numerical Simulations 199
A Reduced Order Model for Preliminary Design and Performance Prediction of Radial Turbopumps 199
Spectral Solution of Reynolds’ Film Lubrication Equation for Finite Length Journal Bearing 194
Identification of Cavitation Instabilities on a Three-Bladed Inducer by Means of Strain Gages 190
Experimental Characterization of Thermal Cavitation Effects on Space Rocket Axial Inducers 188
Performance of a Monopropellant Thruster Prototype Using Advanced Hydrogen Peroxide Catalytic Beds 186
Experimental Campaign on a 98% H2O2 Pulsed Thruster 186
Identification of Cavitation Instabilities on a Three-Bladed Inducer by Means of Strain Gages 185
Endurance Tests on Different Catalytic Beds for H2O2 Monopropellant Thrusters 184
Experimental and numerical study on hydraulic performances of a turbopump with and without an inducer 183
Experimental Campaign on a Green Bipropellant Reaction Control Thruster 183
Development and Testing of Pt/Al2O3 Catalysts for Hydrogen Peroxide Decomposition 182
Cavitation and Flow Instabilities in a 4-Bladed Axial Inducer Designed by Means of a Reduced Order Analytical Model 179
Firing Performance of Advanced Hydrogen Peroxide Catalytic Beds in a Monopropellant Thruster Prototype 177
An Introduction to Cavitation in Inducers and Turbopumps 175
PulCheR-PULSED CHEMICAL ROCKET WITH GREEN HIGH PERFORMANCE PROPELLANTS: 30TH MONTH PROJECT OVERVIEW 175
Latest Activities on Turbopumps at SITAEL with an On Board Acquisition System 168
Experimental Characterization of Thermal Cavitation Effects on Space Rocket Axial Inducers 167
Fluid-Induced Rotordynamic Forces on a Whirling Centrifugal Pump 166
Experimental Characterization of Unsteady Forces Triggered by Cavitation on a Centrifugal Pump 166
A Test Facility for the Lifetime Characterization of Cryogenic High-Speed Bearings 164
Propulsive Performance of a 100 µm Pt/CexZr1-x/Al2O3 Catalytic Bed 162
Experimental Characterization of Unsteady Forces Triggered by Cavitation on a Centrifugal Pump † 162
On the Preliminary Design and Performance Prediction of Centrifugal Turbopumps—Part 1 160
Pulse Mode Operation of a 1 N 98% Hydrogen Peroxide Thruster 159
Thermal Stress Analysis of Ceramic Pellets for Catalysis 158
A Light Unsaturated Hydrocarbon and Hydrogen Peroxide as Future Green Propellants for Bipropellant Thrusters 157
Analysis of Flow Instabilities on a Three-Bladed Axial Inducer in the Fixed and Rotating Frames 156
Design of a Test Setup for the Characterization of the Dynamic Transfer Matrix of Cavitating Inducers 155
Fluid-Induced Rotordynamic Forces on a Whirling Centrifugal Pump 155
Green Propellant Thruster Design for LEO Platforms Active Debris Removal 155
PROPULSIVE PERFORMANCE OF A C3H4/H2O2 ROCKET PROTOTYPE FOR FUTURE GREEN BIPROPELLANT THRUSTERS 154
Dynamics of the Blade Channel of an Inducer under Cavitation-Induced Instabilities 153
Preliminary Screening of Catalytic Beds for Hydrogen Peroxide with Thrust Level Lower Than 0.5 N 152
Additive manufacturing techniques applied to the space industry 152
A Reduced Order Model for Preliminary Design and Performance Prediction of Tapered Inducers 151
Parametric Identification of Rotating Cavitation in a Three-Bladed Axial Inducer 151
Experimental Performance of a Tapered Axial Inducer: Comparison with Analytical Predictions 150
Green Propellants Research at Alta S.p.A 150
Continuous Spectrum of the Rotordynamic Forces on a Four Bladed Inducer 150
Test Bench for the Unsteady Characterization of a Pulsed Green Monopropellant Thruster 150
Thermal Cavitation Instability Analysis in Axial Inducers by Means of Casing And Hub-Mounted Pressure Sensors 150
Conceptual study of technologies enabling novel green expendable upper stages with multi-payload/multi-orbit injection capability 148
Performance Characterization of Pellet Catalytic Beds for Hydrogen Peroxide Monopropellant Rockets 147
Effects of the Leading Edge Shape on the Performance of an Axial Three Bladed Inducer 147
Characterization of the Rotordynamic Forces on Tapered Axial Inducers by Means of a Rotating Dynamometer and High-Speed Movies 146
Propulsive Performance of a 1 N 98% Hydrogen Peroxide Thruster 146
Design and Testing of a 98% H2O2 Pulsed Thruster 145
Design Parameters of Tethered Cable Nets for the Active Removal of Space Debris 145
Flow Instabilities on a Three-Bladed Axial Inducer at Variable Tip Clearance 144
Post-Reaction Characterization of a Pt/CexZrx-1/Al2O3 Catalyst after the Use in a HTP Thruster 143
Dynamics of the Blade Channel of an Inducer Under Cavitation-Induced Instabilities 142
Comparison of Numerical Simulations to a Reduced-Order Model Extended with Splitter Blades 141
RLV applications: challenges and benefits of novel technologies for sustainable main stages 140
An Introduction to Flow-Induced Instabilities in Rocket Engine Inducers and Turbopumps 138
On the Preliminary Design and Performance Prediction of Centrifugal Turbopumps—Part 2 138
Experimental Characterization of the Rotordynamic Forces on Space Rocket Axial Inducers 137
Inducer and Centrifugal Pump Contributions to the Rotordynamic Fluid Forces Acting on a Space Turbopump 135
Experimental and Numerical Study on Cavitation Performances of a Turbopump with and without an Inducer 134
Analysis of Flow Instabilities on a Three-Bladed Axial Inducer in Fixed and Rotating Frames 132
Modelling of deployable cable nets for active space debris removal 131
Effects of the Leading Edge Shape on the Performance of an Axial Three Bladed Inducer 131
Development of hydrogen peroxide rockets at alta S.P.A.: The past, the present and the future 126
Analysis of an Autogenous Propellant Pressurization System for Nuclear Thermal Rocket 122
High Mass Flux Tests on Catalytic Beds for H2O2 Monopropellant Thruster 120
Autonomous Cubesat propulsion for affordable access to space 120
Simulation of Deployable Cable Nets for Active Debris Removal in Space 119
Maximum Likelihood Identification of Cavitation Instabilities in Axial Inducers 118
Totale 20.220
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Categoria #
all - tutte 65.772
article - articoli 0
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 65.772
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20221.242 0 0 46 103 298 183 56 64 91 49 96 256
2022/20231.648 247 198 109 82 142 190 85 137 215 71 131 41
2023/20242.260 232 192 240 207 310 294 123 120 49 145 168 180
2024/20255.890 103 265 144 323 501 622 801 368 482 676 584 1.021
2025/20267.094 322 760 941 603 669 591 1.160 395 478 611 363 201
2026/20271.232 239 487 506 0 0 0 0 0 0 0 0 0
Totale 25.728