CINECA IRIS Institutional Research Information System

PASINI, ANGELO
 Distribuzione geografica
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Continente #
NA - Nord America 10.557
AS - Asia 6.369
EU - Europa 5.946
SA - Sud America 794
AF - Africa 163
OC - Oceania 110
Continente sconosciuto - Info sul continente non disponibili 1
Totale 23.940
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Nazione #
US - Stati Uniti d'America 10.193
IT - Italia 2.430
SG - Singapore 1.679
CN - Cina 1.658
HK - Hong Kong 985
SE - Svezia 731
BR - Brasile 655
DE - Germania 542
VN - Vietnam 512
GB - Regno Unito 407
FR - Francia 385
TR - Turchia 305
IN - India 298
BG - Bulgaria 288
CA - Canada 268
JP - Giappone 211
FI - Finlandia 173
RU - Federazione Russa 168
KR - Corea 167
ES - Italia 149
NL - Olanda 147
UA - Ucraina 146
CH - Svizzera 75
AU - Australia 73
BD - Bangladesh 61
IR - Iran 57
AT - Austria 54
MX - Messico 54
PL - Polonia 53
AR - Argentina 46
TH - Thailandia 46
TW - Taiwan 44
PH - Filippine 43
BE - Belgio 41
MA - Marocco 41
PK - Pakistan 41
IQ - Iraq 38
NZ - Nuova Zelanda 36
PT - Portogallo 36
SA - Arabia Saudita 36
ZA - Sudafrica 35
ID - Indonesia 33
KE - Kenya 26
IE - Irlanda 25
UZ - Uzbekistan 23
VE - Venezuela 21
AE - Emirati Arabi Uniti 19
MY - Malesia 18
CL - Cile 16
CO - Colombia 16
CI - Costa d'Avorio 14
EG - Egitto 13
PE - Perù 13
DZ - Algeria 12
GR - Grecia 12
LT - Lituania 12
AZ - Azerbaigian 11
EC - Ecuador 11
IL - Israele 11
RO - Romania 11
NP - Nepal 10
JO - Giordania 9
TN - Tunisia 9
CZ - Repubblica Ceca 8
PS - Palestinian Territory 8
DO - Repubblica Dominicana 7
HU - Ungheria 7
NO - Norvegia 7
PY - Paraguay 7
EE - Estonia 6
KZ - Kazakistan 6
OM - Oman 6
UY - Uruguay 6
GE - Georgia 5
JM - Giamaica 5
LU - Lussemburgo 5
PA - Panama 5
BH - Bahrain 4
CR - Costa Rica 4
DK - Danimarca 4
HN - Honduras 4
HR - Croazia 4
LK - Sri Lanka 4
MO - Macao, regione amministrativa speciale della Cina 4
AL - Albania 3
BA - Bosnia-Erzegovina 3
KW - Kuwait 3
MK - Macedonia 3
NG - Nigeria 3
NI - Nicaragua 3
SK - Slovacchia (Repubblica Slovacca) 3
SV - El Salvador 3
BJ - Benin 2
BO - Bolivia 2
CG - Congo 2
ET - Etiopia 2
GT - Guatemala 2
KG - Kirghizistan 2
LB - Libano 2
MD - Moldavia 2
Totale 23.908
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Città #
Woodbridge 1.015
Ashburn 968
Dallas 947
Singapore 921
Hong Kong 913
San Jose 674
Fairfield 613
Houston 584
Santa Clara 573
Shanghai 564
Ann Arbor 559
Milan 510
Chandler 383
Beijing 294
Pisa 293
Sofia 288
Seattle 255
Wilmington 247
New York 238
Cambridge 212
Los Angeles 204
Rome 196
Boardman 169
Ottawa 159
Jacksonville 158
Serra 157
Florence 140
Ho Chi Minh City 135
Izmir 134
Princeton 122
Lawrence 116
Lauterbourg 115
Frankfurt am Main 110
Tokyo 109
Hefei 105
Hanoi 100
Nanjing 95
Istanbul 69
Buffalo 68
Council Bluffs 68
Helsinki 65
Dearborn 59
Munich 59
Seoul 58
Medford 54
Paris 54
São Paulo 52
Columbus 47
Bern 46
Ankara 44
Bangkok 43
Southampton 43
Des Moines 42
Redondo Beach 41
Kent 40
London 39
Düsseldorf 38
Orem 38
The Dalles 36
Dong Ket 34
Mumbai 34
Boulder 33
Lucca 33
Turin 33
San Diego 32
Turku 32
Madrid 31
Delft 30
Jüchen 30
Toronto 30
Nanchang 29
Chennai 28
Melbourne 27
Ogden 27
Warsaw 27
Amsterdam 26
Berlin 26
Casablanca 26
Hyderabad 26
Phoenix 26
Pune 26
Shenyang 26
Barcelona 25
Belo Horizonte 25
Bengaluru 25
Nairobi 25
Vienna 25
Changsha 24
Chicago 23
Naples 23
Redwood City 23
Brussels 22
West Lafayette 22
Glasgow 21
Guangzhou 21
Manchester 21
Livorno 20
Tianjin 20
Bologna 19
Dhaka 19
Totale 15.553
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Nome #
Eco-design of future reusable launchers: insight into their life-cycle and atmospheric impact 1.046
Assessment of Propulsion System Architectures for Green Propellants-based Orbital Stages 515
Design of a Modular 1U Propellant Tank for CubeSats HTP Monopropellant Propulsion System 511
Deployable cable nets for active removal of derelict rocket bodies 400
Three-dimensional deployment of cable nets for active removal of space debris 400
LUNANOVA KICK STAGE STUDY: AN OVERVIEW OF THE SYSTEM PROPULSION TRADEOFFS 312
Development of a High Power, Magnetically Shielded, Dual Channel Hall Thruster in The Framework of the TANDEM Project 297
Development of the EXCITE IOD/IOV mission 293
TANDEM: a High Power, Magnetically Shielded Hall Thruster with a Nested Configuration 282
Development of High Speed Hybrid Bearings for Reusable Pump-Fed Liquid Rocket Engines 281
CubeSat Green Propellants AM Tanks: Efficient Designs, Propellant Management, And Chemical Compatibility 276
Nuclear Thermal Propulsion for Earth Orbit and Interplanetary Missions: Challenges and Issues. 270
On the Preliminary Design and Noncavitating Performance of Tapered Axial Inducers 255
Turbopump Design: Comparison of Numerical Simulations to an Already Validated Reduced-Order Model 234
Cavitating Pump Rotordynamic Test Facility at ALTA S.p.A.: Upgraded Capabilities of a Unique Test Rig 232
Experimental Characterization of a 5 N Hydrogen Peroxide Monopropellant Thruster Prototype 226
Performance Modeling and Analysis of H2O2 Catalytic Pellet Reactors 221
Use of Pt/CexZr1-xAl2O3 as Advanced Catalyst for Hydrogen Peroxide Thrusters 221
Testing and Characterization of a Hydrogen Peroxide Monopropellant Thruster 220
Cavitation and Turbopump Hydrodynamics Research at Alta S.P.A. and Pisa University 220
Performance of Different Catalysts Supported on Alumina Spheres for Hydrogen Peroxide Decomposition 217
Design of an Affordable Hydrogen Peroxide Propulsion System for CubeSats 217
Cavitation and Flow Instabilities in a 3- Bladed Axial Inducer Designed by Means of a Reduced Order Analytical Model 216
Rotordynamic Forces on a Four Bladed Inducer 216
Development of Hydrogen Peroxide Rockets at Alta S.p.A.: the Past, the Present and the Future 214
Platinum catalysts development for 98% hydrogen peroxide decomposition in pulsed monopropellant thrusters 213
A Reduced Order Model for Optimal Centrifugal Pump Design 211
Theoretical Optimization of Splitter Blade Geometry in High-Efficiency Centrifugal Turbopumps 211
Continuous Spectrum of the Rotordynamic Forces on a Four Bladed Inducer 209
Inducer and centrifugal pump contributions to the rotordynamic fluid forces acting on a space turbopump 197
Comparative Characterization of Advanced Catalytic Beds for Hydrogen Peroxide Thrusters 196
A Reduced Order Model for Preliminary Design and Performance Prediction of Tapered Inducers: Comparison with Numerical Simulations 194
Maximum Likelihood Identification of Cavitation Instabilities in Axial Inducers 194
A Reduced Order Model for Preliminary Design and Performance Prediction of Radial Turbopumps 192
Identification of Cavitation Instabilities on a Three-Bladed Inducer by Means of Strain Gages 187
Spectral Solution of Reynolds’ Film Lubrication Equation for Finite Length Journal Bearing 186
Experimental Characterization of Thermal Cavitation Effects on Space Rocket Axial Inducers 185
Performance of a Monopropellant Thruster Prototype Using Advanced Hydrogen Peroxide Catalytic Beds 183
Endurance Tests on Different Catalytic Beds for H2O2 Monopropellant Thrusters 180
Experimental Campaign on a 98% H2O2 Pulsed Thruster 177
Identification of Cavitation Instabilities on a Three-Bladed Inducer by Means of Strain Gages 177
Experimental and numerical study on hydraulic performances of a turbopump with and without an inducer 176
Experimental Campaign on a Green Bipropellant Reaction Control Thruster 176
Cavitation and Flow Instabilities in a 4-Bladed Axial Inducer Designed by Means of a Reduced Order Analytical Model 175
An Introduction to Cavitation in Inducers and Turbopumps 169
Firing Performance of Advanced Hydrogen Peroxide Catalytic Beds in a Monopropellant Thruster Prototype 168
Development and Testing of Pt/Al2O3 Catalysts for Hydrogen Peroxide Decomposition 168
PulCheR-PULSED CHEMICAL ROCKET WITH GREEN HIGH PERFORMANCE PROPELLANTS: 30TH MONTH PROJECT OVERVIEW 164
Fluid-Induced Rotordynamic Forces on a Whirling Centrifugal Pump 162
Experimental Characterization of Thermal Cavitation Effects on Space Rocket Axial Inducers 161
Experimental Characterization of Unsteady Forces Triggered by Cavitation on a Centrifugal Pump 158
Experimental Characterization of Unsteady Forces Triggered by Cavitation on a Centrifugal Pump † 158
Propulsive Performance of a 100 µm Pt/CexZr1-x/Al2O3 Catalytic Bed 156
Latest Activities on Turbopumps at SITAEL with an On Board Acquisition System 156
A Test Facility for the Lifetime Characterization of Cryogenic High-Speed Bearings 156
Pulse Mode Operation of a 1 N 98% Hydrogen Peroxide Thruster 155
On the Preliminary Design and Performance Prediction of Centrifugal Turbopumps—Part 1 155
A Light Unsaturated Hydrocarbon and Hydrogen Peroxide as Future Green Propellants for Bipropellant Thrusters 152
Thermal Stress Analysis of Ceramic Pellets for Catalysis 151
Analysis of Flow Instabilities on a Three-Bladed Axial Inducer in the Fixed and Rotating Frames 148
Fluid-Induced Rotordynamic Forces on a Whirling Centrifugal Pump 148
Green Propellant Thruster Design for LEO Platforms Active Debris Removal 148
Design of a Test Setup for the Characterization of the Dynamic Transfer Matrix of Cavitating Inducers 147
Thermal Cavitation Instability Analysis in Axial Inducers by Means of Casing And Hub-Mounted Pressure Sensors 147
A Reduced Order Model for Preliminary Design and Performance Prediction of Tapered Inducers 146
PROPULSIVE PERFORMANCE OF A C3H4/H2O2 ROCKET PROTOTYPE FOR FUTURE GREEN BIPROPELLANT THRUSTERS 146
Test Bench for the Unsteady Characterization of a Pulsed Green Monopropellant Thruster 146
Continuous Spectrum of the Rotordynamic Forces on a Four Bladed Inducer 145
Experimental Performance of a Tapered Axial Inducer: Comparison with Analytical Predictions 144
Effects of the Leading Edge Shape on the Performance of an Axial Three Bladed Inducer 144
Dynamics of the Blade Channel of an Inducer under Cavitation-Induced Instabilities 144
Additive manufacturing techniques applied to the space industry 144
Preliminary Screening of Catalytic Beds for Hydrogen Peroxide with Thrust Level Lower Than 0.5 N 143
Parametric Identification of Rotating Cavitation in a Three-Bladed Axial Inducer 143
Green Propellants Research at Alta S.p.A 142
Performance Characterization of Pellet Catalytic Beds for Hydrogen Peroxide Monopropellant Rockets 142
Characterization of the Rotordynamic Forces on Tapered Axial Inducers by Means of a Rotating Dynamometer and High-Speed Movies 140
Design and Testing of a 98% H2O2 Pulsed Thruster 139
Propulsive Performance of a 1 N 98% Hydrogen Peroxide Thruster 137
Dynamics of the Blade Channel of an Inducer Under Cavitation-Induced Instabilities 137
Flow Instabilities on a Three-Bladed Axial Inducer at Variable Tip Clearance 134
RLV applications: challenges and benefits of novel technologies for sustainable main stages 134
Post-Reaction Characterization of a Pt/CexZrx-1/Al2O3 Catalyst after the Use in a HTP Thruster 133
On the Preliminary Design and Performance Prediction of Centrifugal Turbopumps—Part 2 133
An Introduction to Flow-Induced Instabilities in Rocket Engine Inducers and Turbopumps 132
Experimental and Numerical Study on Cavitation Performances of a Turbopump with and without an Inducer 129
Comparison of Numerical Simulations to a Reduced-Order Model Extended with Splitter Blades 128
Inducer and Centrifugal Pump Contributions to the Rotordynamic Fluid Forces Acting on a Space Turbopump 126
Conceptual study of technologies enabling novel green expendable upper stages with multi-payload/multi-orbit injection capability 126
Effects of the Leading Edge Shape on the Performance of an Axial Three Bladed Inducer 124
Experimental Characterization of the Rotordynamic Forces on Space Rocket Axial Inducers 124
Analysis of Flow Instabilities on a Three-Bladed Axial Inducer in Fixed and Rotating Frames 122
Modelling of deployable cable nets for active space debris removal 121
Development of hydrogen peroxide rockets at alta S.P.A.: The past, the present and the future 121
null 116
Maximum Likelihood Identification of Cavitation Instabilities in Axial Inducers 115
High Mass Flux Tests on Catalytic Beds for H2O2 Monopropellant Thruster 114
Concurrent theoretical, experimental and numerical analyses of mixed-flow turbopump design 113
Analysis of an Autogenous Propellant Pressurization System for Nuclear Thermal Rocket 113
Simulation of Deployable Cable Nets for Active Debris Removal in Space 112
Totale 19.290
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Categoria #
all - tutte 60.809
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 60.809
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021153 0 0 0 0 0 0 0 0 0 0 0 153
2021/20221.369 49 78 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
2025/20266.959 322 760 941 603 669 591 1.160 395 478 611 363 66
Totale 24.361