CINECA IRIS Institutional Research Information System

PASINI, ANGELO
 Distribuzione geografica
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Continente #
NA - Nord America 6.018
EU - Europa 3.722
AS - Asia 1.374
OC - Oceania 54
AF - Africa 39
SA - Sud America 15
Totale 11.222
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Nazione #
US - Stati Uniti d'America 5.854
IT - Italia 1.654
SE - Svezia 705
CN - Cina 499
DE - Germania 303
BG - Bulgaria 287
SG - Singapore 238
TR - Turchia 183
CA - Canada 164
GB - Regno Unito 153
UA - Ucraina 115
VN - Vietnam 112
IN - India 91
FR - Francia 90
FI - Finlandia 74
JP - Giappone 72
ES - Italia 69
HK - Hong Kong 62
CH - Svizzera 52
NL - Olanda 49
RU - Federazione Russa 46
IR - Iran 36
AU - Australia 31
KR - Corea 31
AT - Austria 30
NZ - Nuova Zelanda 23
PL - Polonia 23
BE - Belgio 22
CI - Costa d'Avorio 14
PT - Portogallo 11
TW - Taiwan 10
IE - Irlanda 8
PK - Pakistan 8
ZA - Sudafrica 8
BR - Brasile 7
EG - Egitto 6
TH - Thailandia 6
AE - Emirati Arabi Uniti 5
EE - Estonia 5
ID - Indonesia 5
NO - Norvegia 5
CZ - Repubblica Ceca 4
DZ - Algeria 4
AR - Argentina 3
CO - Colombia 3
GR - Grecia 3
IL - Israele 3
MA - Marocco 3
PS - Palestinian Territory 3
RO - Romania 3
SA - Arabia Saudita 3
SK - Slovacchia (Repubblica Slovacca) 3
GE - Georgia 2
HR - Croazia 2
MD - Moldavia 2
NG - Nigeria 2
SN - Senegal 2
AL - Albania 1
AM - Armenia 1
DK - Danimarca 1
EC - Ecuador 1
KZ - Kazakistan 1
LI - Liechtenstein 1
LK - Sri Lanka 1
LU - Lussemburgo 1
MO - Macao, regione amministrativa speciale della Cina 1
MY - Malesia 1
VE - Venezuela 1
Totale 11.222
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Città #
Woodbridge 1.015
Fairfield 613
Houston 570
Ann Arbor 557
Milan 433
Chandler 383
Ashburn 340
Sofia 287
Seattle 250
Wilmington 246
Cambridge 211
New York 186
Beijing 170
Pisa 162
Jacksonville 157
Ottawa 153
Serra 153
Izmir 133
Princeton 121
Lawrence 115
Florence 102
Nanjing 92
Rome 90
Singapore 75
Frankfurt am Main 62
Dearborn 59
Medford 52
Bern 46
Hong Kong 42
Des Moines 40
Kent 40
Southampton 36
Dong Ket 34
Boulder 32
San Diego 31
Jüchen 30
Nanchang 29
Ogden 27
Düsseldorf 26
Los Angeles 25
Pune 25
Redwood City 23
Shenyang 23
Boardman 22
Paris 21
Barcelona 18
Luft 18
Tianjin 18
Ankara 16
Changsha 16
Hebei 16
Melbourne 16
Shanghai 16
Baltimore 15
Brussels 15
Kunming 15
Livorno 15
Abidjan 14
Madrid 14
Napier City 14
Delft 13
Salò 13
San Jose 13
Tokyo 13
Lecco 12
London 12
West Lafayette 12
Xian 12
Magenta 11
Munich 11
Graz 10
Hangzhou 10
Bengaluru 9
Hefei 9
Norwalk 9
Saronno 9
Bari 8
Bologna 8
Colindale 8
Guangzhou 8
Islamabad 8
Jiaxing 8
Kocaeli 8
Les Mureaux 8
Naples 8
Santa Clara 8
Seoul 8
Toulouse 8
Turin 8
Vienna 8
Auburn Hills 7
Costa Mesa 7
Davis 7
Esfahan 7
Germering 7
Indiana 7
Taranto 7
Tehran 7
Utrecht 7
Warsaw 7
Totale 7.935
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Nome #
Eco-design of future reusable launchers: insight into their life-cycle and atmospheric impact 265
Design of a Modular 1U Propellant Tank for CubeSats HTP Monopropellant Propulsion System 213
Testing and Characterization of a Hydrogen Peroxide Monopropellant Thruster 164
Cavitation and Flow Instabilities in a 3- Bladed Axial Inducer Designed by Means of a Reduced Order Analytical Model 163
Performance Modeling and Analysis of H2O2 Catalytic Pellet Reactors 161
Use of Pt/CexZr1-xAl2O3 as Advanced Catalyst for Hydrogen Peroxide Thrusters 161
Experimental Characterization of a 5 N Hydrogen Peroxide Monopropellant Thruster Prototype 160
Performance of Different Catalysts Supported on Alumina Spheres for Hydrogen Peroxide Decomposition 159
A Reduced Order Model for Optimal Centrifugal Pump Design 157
Continuous Spectrum of the Rotordynamic Forces on a Four Bladed Inducer 156
Cavitating Pump Rotordynamic Test Facility at ALTA S.p.A.: Upgraded Capabilities of a Unique Test Rig 156
On the Preliminary Design and Noncavitating Performance of Tapered Axial Inducers 153
Assessment of Propulsion System Architectures for Green Propellants-based Orbital Stages 144
A Reduced Order Model for Preliminary Design and Performance Prediction of Tapered Inducers: Comparison with Numerical Simulations 144
Platinum catalysts development for 98% hydrogen peroxide decomposition in pulsed monopropellant thrusters 144
Development of Hydrogen Peroxide Rockets at Alta S.p.A.: the Past, the Present and the Future 144
A Reduced Order Model for Preliminary Design and Performance Prediction of Radial Turbopumps 143
Comparative Characterization of Advanced Catalytic Beds for Hydrogen Peroxide Thrusters 138
Development of High Speed Hybrid Bearings for Reusable Pump-Fed Liquid Rocket Engines 136
Experimental Characterization of Thermal Cavitation Effects on Space Rocket Axial Inducers 134
An Introduction to Cavitation in Inducers and Turbopumps 131
Performance of a Monopropellant Thruster Prototype Using Advanced Hydrogen Peroxide Catalytic Beds 128
Endurance Tests on Different Catalytic Beds for H2O2 Monopropellant Thrusters 128
Cavitation and Turbopump Hydrodynamics Research at Alta S.P.A. and Pisa University 125
Rotordynamic Forces on a Four Bladed Inducer 125
Cavitation and Flow Instabilities in a 4-Bladed Axial Inducer Designed by Means of a Reduced Order Analytical Model 120
Fluid-Induced Rotordynamic Forces on a Whirling Centrifugal Pump 119
Experimental Characterization of Thermal Cavitation Effects on Space Rocket Axial Inducers 119
Development of a High Power, Magnetically Shielded, Dual Channel Hall Thruster in The Framework of the TANDEM Project 118
Inducer and centrifugal pump contributions to the rotordynamic fluid forces acting on a space turbopump 117
Firing Performance of Advanced Hydrogen Peroxide Catalytic Beds in a Monopropellant Thruster Prototype 116
null 116
null 112
Propulsive Performance of a 100 µm Pt/CexZr1-x/Al2O3 Catalytic Bed 110
A Light Unsaturated Hydrocarbon and Hydrogen Peroxide as Future Green Propellants for Bipropellant Thrusters 109
null 108
Experimental Campaign on a Green Bipropellant Reaction Control Thruster 108
Development and Testing of Pt/Al2O3 Catalysts for Hydrogen Peroxide Decomposition 107
Experimental Characterization of Unsteady Forces Triggered by Cavitation on a Centrifugal Pump 107
Theoretical Optimization of Splitter Blade Geometry in High-Efficiency Centrifugal Turbopumps 107
On the Preliminary Design and Performance Prediction of Centrifugal Turbopumps—Part 1 106
Identification of Cavitation Instabilities on a Three-Bladed Inducer by Means of Strain Gages 103
null 101
Dynamics of the Blade Channel of an Inducer under Cavitation-Induced Instabilities 100
Fluid-Induced Rotordynamic Forces on a Whirling Centrifugal Pump 100
Green Propellants Research at Alta S.p.A 99
Continuous Spectrum of the Rotordynamic Forces on a Four Bladed Inducer 99
Characterization of the Rotordynamic Forces on Tapered Axial Inducers by Means of a Rotating Dynamometer and High-Speed Movies 98
Turbopump Design: Comparison of Numerical Simulations to an Already Validated Reduced-Order Model 96
Effects of the Leading Edge Shape on the Performance of an Axial Three Bladed Inducer 95
On the Preliminary Design and Performance Prediction of Centrifugal Turbopumps—Part 2 95
Pulse Mode Operation of a 1 N 98% Hydrogen Peroxide Thruster 94
A Reduced Order Model for Preliminary Design and Performance Prediction of Tapered Inducers 93
Performance Characterization of Pellet Catalytic Beds for Hydrogen Peroxide Monopropellant Rockets 93
Thermal Stress Analysis of Ceramic Pellets for Catalysis 92
Post-Reaction Characterization of a Pt/CexZrx-1/Al2O3 Catalyst after the Use in a HTP Thruster 91
An Introduction to Flow-Induced Instabilities in Rocket Engine Inducers and Turbopumps 89
Test Bench for the Unsteady Characterization of a Pulsed Green Monopropellant Thruster 89
LUNANOVA KICK STAGE STUDY: AN OVERVIEW OF THE SYSTEM PROPULSION TRADEOFFS 89
Analysis of Flow Instabilities on a Three-Bladed Axial Inducer in the Fixed and Rotating Frames 86
Design and Testing of a 98% H2O2 Pulsed Thruster 86
null 85
PulCheR-PULSED CHEMICAL ROCKET WITH GREEN HIGH PERFORMANCE PROPELLANTS: 30TH MONTH PROJECT OVERVIEW 85
Design of an Affordable Hydrogen Peroxide Propulsion System for CubeSats 85
TANDEM: a High Power, Magnetically Shielded Hall Thruster with a Nested Configuration 84
Experimental Performance of a Tapered Axial Inducer: Comparison with Analytical Predictions 84
Experimental and numerical study on hydraulic performances of a turbopump with and without an inducer 84
null 83
PROPULSIVE PERFORMANCE OF A C3H4/H2O2 ROCKET PROTOTYPE FOR FUTURE GREEN BIPROPELLANT THRUSTERS 82
Latest Activities on Turbopumps at SITAEL with an On Board Acquisition System 82
Design of a Test Setup for the Characterization of the Dynamic Transfer Matrix of Cavitating Inducers 80
Experimental Characterization of the Rotordynamic Forces on Space Rocket Axial Inducers 77
Propulsive Performance of a 1 N 98% Hydrogen Peroxide Thruster 77
Effects of the Leading Edge Shape on the Performance of an Axial Three Bladed Inducer 76
null 76
Additive manufacturing techniques applied to the space industry 76
Experimental Characterization of Unsteady Forces Triggered by Cavitation on a Centrifugal Pump † 75
null 74
Maximum Likelihood Identification of Cavitation Instabilities in Axial Inducers 74
null 73
Flow Instabilities on a Three-Bladed Axial Inducer at Variable Tip Clearance 72
null 71
Identification of Cavitation Instabilities on a Three-Bladed Inducer by Means of Strain Gages 71
Inducer and Centrifugal Pump Contributions to the Rotordynamic Fluid Forces Acting on a Space Turbopump 70
Thermal Cavitation Instability Analysis in Axial Inducers by Means of Casing And Hub-Mounted Pressure Sensors 70
null 69
PulCheR-Pulsed Chemical Rocket with Green High Performance Propellants: Second Year Project Overview 67
null 67
null 66
Experimental Campaign on a 98% H2O2 Pulsed Thruster 66
High Mass Flux Tests on Catalytic Beds for H2O2 Monopropellant Thruster 64
Development of hydrogen peroxide rockets at alta S.P.A.: The past, the present and the future 64
Rotordynamic Forces on a Three Bladed Inducer 62
Control of Operation Mode Transition in Dual-Bell Nozzle with Film Cooling 62
Spectral Solution of Reynolds’ Film Lubrication Equation for Finite Length Journal Bearing 61
A Test Facility for the Lifetime Characterization of Cryogenic High-Speed Bearings 61
null 59
null 52
Autonomous Cubesat propulsion for affordable access to space 51
Green Propellant Thruster Design for LEO Platforms Active Debris Removal 50
Totale 10.306
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Categoria #
all - tutte 28.648
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 28.648
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20201.841 231 131 107 144 149 188 193 163 186 107 147 95
2020/20211.019 78 58 48 56 139 43 85 83 133 70 73 153
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
2024/202582 82 0 0 0 0 0 0 0 0 0 0 0
Totale 11.594