statistiche ricercatore

Nazione	#
US - Stati Uniti d'America	1.820
IT - Italia	596
DE - Germania	394
CN - Cina	318
FR - Francia	262
GB - Regno Unito	254
SG - Singapore	175
UA - Ucraina	117
RU - Federazione Russa	84
NL - Olanda	52
IE - Irlanda	43
KR - Corea	36
TR - Turchia	30
BR - Brasile	28
CH - Svizzera	28
IN - India	27
MY - Malesia	18
FI - Finlandia	17
HK - Hong Kong	16
ES - Italia	15
VN - Vietnam	12
AR - Argentina	9
AT - Austria	8
BE - Belgio	8
CA - Canada	8
PL - Polonia	7
PT - Portogallo	7
EU - Europa	5
GR - Grecia	5
JO - Giordania	5
SE - Svezia	5
ID - Indonesia	4
IL - Israele	4
JP - Giappone	4
IR - Iran	3
NG - Nigeria	3
SK - Slovacchia (Repubblica Slovacca)	3
TT - Trinidad e Tobago	3
AU - Australia	2
BD - Bangladesh	2
CL - Cile	2
CO - Colombia	2
CR - Costa Rica	2
EC - Ecuador	2
EE - Estonia	2
GP - Guadalupe	2
NZ - Nuova Zelanda	2
RO - Romania	2
BH - Bahrain	1
CZ - Repubblica Ceca	1
EG - Egitto	1
HU - Ungheria	1
IQ - Iraq	1
LU - Lussemburgo	1
MA - Marocco	1
MU - Mauritius	1
MX - Messico	1
SD - Sudan	1
SN - Senegal	1
VE - Venezuela	1
ZA - Sudafrica	1
Totale	4.466

Nome	#
Cooperative Deployment of satellite formation into Highly Elliptic Orbit	480
Indirect Optimization of Satellite Deployment into a Highly Elliptic Orbit	436
Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper Stage	379
Indirect Optimization of Asteroid Deflection Missions with Electric Propulsion	329
Comparison of Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper-Stage	309
Deployment of a Two-Spacecraft Formation into a Highly Elliptic Orbit with Collision Avoidance	286
Tour of Jupiter Galilean moons: Winning solution of GTOC6	282
Optimization of Open Rotor Engines for Civil Aircraft Using a Cooperative Evolutionary Method	280
Hybrid rocket upper stage optimization: effects of grain geometry	277
Effects of Limitation of Nozzle Flow Separation on Launcher Performance	260
Effects of limitation of nozzle flow separation on launcher performance	259
Evolutionary optimization of interplanetary trajectories: improvements from initial diversification	242
GTOC5: Results from the Politecnico di Torino and Università di Roma Sapienza	230
Optimal Cooperative Deployment of a Two-Satellite Formation into a Highly Elliptic Orbit	220
Indirect Optimization of Robust Orbit Transfer Considering Thruster Underperformance	132
Missions for Asteroid Insertion into Earth-Mars Cycler	93
Totale	4.494

	Totale	Lug	Ago	Sett	Ott	Nov	Dic	Gen	Feb	Mar	Apr	Mag	Giu
2020/2021	119	0	0	0	0	11	19	6	22	6	26	20	9
2021/2022	215	9	12	22	17	17	17	15	4	24	16	18	44
2022/2023	329	26	52	8	21	26	43	62	10	31	0	9	41
2023/2024	137	8	16	8	8	11	8	10	24	8	4	13	19
2024/2025	296	8	46	30	25	44	13	7	13	37	14	26	33
2025/2026	309	62	75	51	82	39	0	0	0	0	0	0	0
Totale													4.494

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