statistiche ricercatore

Nazione	#
US - Stati Uniti d'America	1.811
IT - Italia	595
DE - Germania	394
CN - Cina	304
FR - Francia	260
GB - Regno Unito	254
UA - Ucraina	117
SG - Singapore	105
RU - Federazione Russa	84
NL - Olanda	52
IE - Irlanda	43
KR - Corea	36
TR - Turchia	30
CH - Svizzera	28
IN - India	27
BR - Brasile	23
MY - Malesia	18
FI - Finlandia	17
ES - Italia	15
HK - Hong Kong	14
AT - Austria	8
BE - Belgio	8
CA - Canada	8
PL - Polonia	7
PT - Portogallo	7
AR - Argentina	6
EU - Europa	5
GR - Grecia	5
JO - Giordania	5
SE - Svezia	5
IL - Israele	4
JP - Giappone	4
ID - Indonesia	3
IR - Iran	3
NG - Nigeria	3
SK - Slovacchia (Repubblica Slovacca)	3
TT - Trinidad e Tobago	3
VN - Vietnam	3
AU - Australia	2
BD - Bangladesh	2
CL - Cile	2
EC - Ecuador	2
EE - Estonia	2
GP - Guadalupe	2
RO - Romania	2
BH - Bahrain	1
CO - Colombia	1
CR - Costa Rica	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
NZ - Nuova Zelanda	1
SD - Sudan	1
ZA - Sudafrica	1
Totale	4.345

Nome	#
Cooperative Deployment of satellite formation into Highly Elliptic Orbit	469
Indirect Optimization of Satellite Deployment into a Highly Elliptic Orbit	427
Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper Stage	374
Indirect Optimization of Asteroid Deflection Missions with Electric Propulsion	320
Comparison of Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper-Stage	304
Deployment of a Two-Spacecraft Formation into a Highly Elliptic Orbit with Collision Avoidance	278
Tour of Jupiter Galilean moons: Winning solution of GTOC6	276
Hybrid rocket upper stage optimization: effects of grain geometry	272
Optimization of Open Rotor Engines for Civil Aircraft Using a Cooperative Evolutionary Method	271
Effects of Limitation of Nozzle Flow Separation on Launcher Performance	252
Effects of limitation of nozzle flow separation on launcher performance	251
Evolutionary optimization of interplanetary trajectories: improvements from initial diversification	236
GTOC5: Results from the Politecnico di Torino and Università di Roma Sapienza	226
Optimal Cooperative Deployment of a Two-Satellite Formation into a Highly Elliptic Orbit	211
Indirect Optimization of Robust Orbit Transfer Considering Thruster Underperformance	120
Missions for Asteroid Insertion into Earth-Mars Cycler	86
Totale	4.373

	Totale	Lug	Ago	Sett	Ott	Nov	Dic	Gen	Feb	Mar	Apr	Mag	Giu
2020/2021	182	0	0	0	63	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	188	62	75	51	0	0	0	0	0	0	0	0	0
Totale													4.373

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