statistiche ricercatore

Continente	#
NA - Nord America	2.060
EU - Europa	2.009
AS - Asia	1.081
SA - Sud America	63
Continente sconosciuto - Info sul continente non disponibili	28
AF - Africa	16
OC - Oceania	4
Totale	5.261

Nazione	#
US - Stati Uniti d'America	2.034
IT - Italia	604
DE - Germania	401
CN - Cina	329
FR - Francia	286
VN - Vietnam	260
GB - Regno Unito	254
SG - Singapore	242
RU - Federazione Russa	123
UA - Ucraina	119
NL - Olanda	53
HK - Hong Kong	51
KR - Corea	51
IE - Irlanda	43
IN - India	42
BR - Brasile	40
TR - Turchia	33
CH - Svizzera	30
FI - Finlandia	18
MY - Malesia	18
ES - Italia	16
AR - Argentina	12
CA - Canada	12
AT - Austria	9
BE - Belgio	8
PH - Filippine	8
PL - Polonia	7
PT - Portogallo	7
TW - Taiwan	7
BD - Bangladesh	6
ID - Indonesia	6
EU - Europa	5
GR - Grecia	5
JM - Giamaica	5
JO - Giordania	5
SE - Svezia	5
IL - Israele	4
IQ - Iraq	4
JP - Giappone	4
EC - Ecuador	3
IR - Iran	3
MA - Marocco	3
NG - Nigeria	3
PK - Pakistan	3
SK - Slovacchia (Repubblica Slovacca)	3
SN - Senegal	3
TH - Thailandia	3
TT - Trinidad e Tobago	3
AU - Australia	2
CL - Cile	2
CO - Colombia	2
CR - Costa Rica	2
EE - Estonia	2
GP - Guadalupe	2
HU - Ungheria	2
MX - Messico	2
NZ - Nuova Zelanda	2
PY - Paraguay	2
RO - Romania	2
VE - Venezuela	2
ZA - Sudafrica	2
AZ - Azerbaigian	1
BH - Bahrain	1
BW - Botswana	1
BY - Bielorussia	1
CZ - Repubblica Ceca	1
EG - Egitto	1
LU - Lussemburgo	1
MU - Mauritius	1
NP - Nepal	1
OM - Oman	1
PS - Palestinian Territory	1
SD - Sudan	1
UG - Uganda	1
UZ - Uzbekistan	1
Totale	5.233

Nome	#
Cooperative Deployment of satellite formation into Highly Elliptic Orbit	589
Indirect Optimization of Satellite Deployment into a Highly Elliptic Orbit	488
Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper Stage	422
Indirect Optimization of Asteroid Deflection Missions with Electric Propulsion	364
Comparison of Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper-Stage	345
Tour of Jupiter Galilean moons: Winning solution of GTOC6	344
Effects of Limitation of Nozzle Flow Separation on Launcher Performance	333
Deployment of a Two-Spacecraft Formation into a Highly Elliptic Orbit with Collision Avoidance	331
Optimization of Open Rotor Engines for Civil Aircraft Using a Cooperative Evolutionary Method	328
Hybrid rocket upper stage optimization: effects of grain geometry	324
Effects of limitation of nozzle flow separation on launcher performance	294
Evolutionary optimization of interplanetary trajectories: improvements from initial diversification	276
Optimal Cooperative Deployment of a Two-Satellite Formation into a Highly Elliptic Orbit	261
GTOC5: Results from the Politecnico di Torino and Università di Roma Sapienza	261
Indirect Optimization of Robust Orbit Transfer Considering Thruster Underperformance	181
Missions for Asteroid Insertion into Earth-Mars Cycler	120
Totale	5.261

	Totale	Lug	Ago	Sett	Ott	Nov	Dic	Gen	Feb	Mar	Apr	Mag	Giu
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	1.059	62	75	51	82	63	75	224	62	190	110	20	45
2026/2027	17	17	0	0	0	0	0	0	0	0	0	0	0
Totale													5.261

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