Publication Date:
2006-02-14
Description:
Structurally efficient ways to support the large solar arrays (3,716 square meters which are currently considered for space station use) are examined. An erectable truss concept is presented for the on orbit construction of winged solar arrays. The means for future growth, maintenance, and repair are integrally designed into this concept. Results from parametric studies, which highlight the physical and structural differences between various configuration options are presented. Consideration is given to both solar blanket and hard panel arrays.
Keywords:
ENERGY PRODUCTION AND CONVERSION
Type:
NASA. Lewis Research Center Space Photovoltaic Res. and Technol. 1983; p 182-192
Format:
text