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BIBLIOGRAFIA
[1] W. J. Larson, J. R. Wertz; Space Mission Analysis and Design, second edition; Microcosm, Inc., Torrance, CA; Kluwer Academic Publishers, Dordrecht, NE; 1992.
[2] M. D. Griffin, J. R. French; Space Vehicle Design; AIAA Education Series, Washington, DC; 1991.
[3] P. Sanz-Aranguez Sanz, T. Elices Concha; Vehiculos Espaciales; Escuela Técni-ca Superior de Ingenieros Aeronáuticos, Sección de PubliTécni-caciones, Madrid, E-spaña; 1999.
[4] L.G. Blomberg; Micro-satellite Mission Analysis: Theory Overview and Some Examples; KTH Report ALP-2003-103; Alfvén Laboratory; Royal Institute of Technology Stockholm, Sweden; March 2003.
[5] C. A. Kluever, S. R. Oleson; Direct Approach for Computing Near-Optimal Low-Thrust Earth-Orbit Transfers; Journal of Spacecraft and Rockets, Vol. 35, No. 4: July-August 1998.
[6] Mengali G.; Meccanica del volo spaziale ; Edizioni Plus Università di Pisa; Pisa, Italia; Novembre 2001
[7] F. Ceccanti; Sistema Propulsivo FEEP per Microsatelliti Basati sulla Piataforma MITA; Tesi di Laurea in Ing. Aerospaziale, Indirizzo Spaziale; Università degli Studi di Pisa, Dip. Ing Aerospaziale; Centrospazio, Pisa, Italia; 1999.
[8] Vega User’s Manual; Arianepace; Marzo 2003.
[9] T.N. Edelbaum; Propulsion requirements for controllable satellites; ARS Journal Agosto 1961 Pag. 1079-1089 .
[10] CEOS Handbook; ESA Publications 2002.
[11] Sommer M. , Rieve P.; First Multispectral Diode Color Imager With Three Color Recognition And Color;1999 IEEE Workshop on CCDs and Advanced Im-age Sensor; Nagano, Giappone, Giugno 10-12, 1999.
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[12] Introduction to Hyperspectral imagery; MicroImages Inc.
[13] Jacobsen, Karsten; Status and tendency of sensors for mapping; University of Hannover, Germany.
[14] Nieke J., Schwarzer H.; Imaging of Spaceborn and Airborne Sensor Systems in the beginning of the next century; DLR- German Aereospace Research Estab-lishment.
[15] Lencioni D.E., Digenis C.J.; Design and Performance of the EO-1 Advanced Land Imager; Massachusetts Institute of Technology – Lincoln Laboratory, USA. [16] Mike Cutter;Compact High Resolution Imaging
Spectrome-ter(CHRIS);siraelectro-optics
[17] The Galilei Project – Galileo Design Consolidation
[18] MEPS EP Technology assessment technical note; ALTA Srl [19] http://www.kerc.msk.ru
[20] http://www.spectrolab.com/DataSheets/TJCell/tj.pdf
[21] Agrawal B.N.; Design of Geosynchronous Spacecraft; Prentice Hall, June 1986.
[22] http://www.saftbatteries.com/130-Catalogue/PDF/space_lithium.pdf [23] http://www.alcatel.com/space/obeqpt/bus /mechani/b302.pdf
[24] Grastataro C.I.,Butler T.A.; Development of a composite satellite structure for Forté; Los Alamos National Laboratory, USA.
