Design concept and feasibility study of a flexible deployable, solar panel generator used on a teledetection satellite

Details Design concept and feasibility study of a flexible deployable, solar panel generator used on a teledetection satellite Design concept and feasibility study of a flexible deployable, solar panel generator used on a teledetection satellite

Sep 1978

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1978snia.rept.....b&link_type=abstract

Final Report Societe Nationale Industrielle Aerospatiale, Cannes (France). Div. Systemes Balistiques et Spatiaux.

Computer Science

European Space Programs, Folding Structures, Solar Generators, Spacecraft Power Supplies, Artificial Satellites, Design Analysis, Flexible Bodies, Solar Cells

Scientific paper

The initial project concept and program for the development of 1.5 kW and 3 kW solar panels are presented. The final project objective is a twice folding 6 kW peak output solar generator to be used on a European earth observation satellite. The experience germed with the ISLA solar panel and with the space telescope is shown to be related to this project. The design of all components is discussed in detail and the planning of the successive development phases is described.

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