Computer Science
Scientific paper
May 1993
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1993stin...9326703c&link_type=abstract
Presented at the 23rd IEEE Photovoltaic Specialists Conference, Louisville, KY, 10-14 May, 1993; sponsored by the Electron Devic
Computer Science
Carbon Fibers, Electric Power, Fiber Composites, Photovoltaic Cells, Solar Arrays, Spacecraft Power Supplies, Amorphous Silicon, Catenaries, Gallium Arsenides, Planetary Bases, Solar Radiation, Structural Design
Scientific paper
To provide electrical power during an exploration mission to Mars, a deployable tent-shaped structure with a flexible photovoltaic (PV) blanket is proposed. The array is designed with a self-deploying mechanism utilizing pressurized gas expansion. The structural design for the array uses a combination of cables, beams, and columns to support and deploy the PV blanket. Under the force of gravity, a cable carrying a uniform load will take the shape of a catenary curve. A catenary-tent collector is self shading which must be taken into account in the solar radiation calculation. The shape and the area of the shadow on the array was calculated and used in the determination of the global irradiance on the array. The PV blanket shape and structure dimensions were optimized to achieve a configuration which maximizes the specific power (W/kg). The optimization was performed for three types of PV blankets (silicon, gallium arsenide over germanium, and amorphous silicon) and two types of structural materials (carbon composite and arimid fiber composite). The results show that the catenary shape of the PV blanket corresponding to zero end angle at the base with respect to the horizontal results in the highest specific power. The tent angle is determined by optimizing the specific mass and the output power for maximum specific power. The combination of carbon fiber structural material and amorphous silicon blanket produces the highest specific power.
Appelbaum Joseph
Colozza Anthony J.
Crutchik Marcos
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