MORETTO, FEDERICO
 Distribuzione geografica
Continente #
NA - Nord America 513
EU - Europa 128
AS - Asia 51
Totale 692
Nazione #
US - Stati Uniti d'America 511
DE - Germania 63
CN - Cina 44
IT - Italia 20
FI - Finlandia 18
GB - Regno Unito 10
FR - Francia 5
SE - Svezia 5
UA - Ucraina 4
IN - India 3
KR - Corea 3
CA - Canada 2
IE - Irlanda 2
NL - Olanda 1
TW - Taiwan 1
Totale 692
Città #
Chandler 120
Fairfield 60
Woodbridge 56
Ann Arbor 40
Cambridge 35
Seattle 28
Wilmington 25
Ashburn 21
Houston 19
Medford 15
Princeton 15
Beijing 14
Jacksonville 13
Roxbury 12
Nanjing 11
Nürnberg 8
Boardman 7
Des Moines 6
Redwood City 6
Helsinki 4
Jinan 4
Nanchang 4
Norwalk 4
San Diego 4
Shenyang 4
Seoul 3
Spinea 3
Changsha 2
Dublin 2
Hangzhou 2
Jiaxing 2
Rome 2
Alghero 1
Borås 1
Bremen 1
Calgary 1
Dallas 1
Landshut 1
Lendinara 1
London 1
Martignacco 1
Massy 1
Munich 1
Nashua 1
Padova 1
Stuttgart 1
Tianjin 1
Venezia 1
Totale 567
Nome #
Numerical Modeling of Paraffin-Based Fuels Behavior 85
SPONGE: a Sounding Rocket Experiment for PMDs 77
Optimization of a H2O2 Gas Generator for a Hybrid Rocket Engine 67
The SPONGE rexus project: Overview of a sounding rocket experiment for PMDs 64
Feasibility Study for a Throttleable Hybrid Rocket Motor for Soft Landing 55
Experimental Characterization of a Hydrogen Peroxide Simulator 53
Development and Flight Testing of a Hybrid Rocket Booster for UAV Assisted Take Off 45
Numerical and Experimental Activities in Support of the Development of Hybrid Rocket Engine for Soft-Landing Applications 42
Feasibility Study for Throttleable Hybrid Rocket Motor for Soft Landing 38
Analysis of Fluid-dynamic Systems to Increase Combustion Efficiency in Hybrid Rockets 34
Feasibility Study of Hybrid Propulsion System for Sounding Rocket Application 33
Numerical and Experimental Activities in Support of the Development of Hybrid-Rocket Engine for softlanding applications 29
Testing of a Hydrogen Peroxide Simulator for a Hybrid Rocket Engine 28
Performance Characterization of Propulsion Systems for Spacecraft Applications 26
Development of 20 kN hybrid rocket booster 22
Totale 698
Categoria #
all - tutte 1392
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 1392


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2017/201811 0000 00 01 00100
2018/201957 4031 41 14 114168
2019/2020161 25637 188 1221 1713283
2020/2021106 26714 128 716 113137
2021/2022113 02050 95 113 103839
2022/2023160 4629521 2726 15 0000
Totale 698