b. Weight Estimates In order to encompass the greatest conceivable range of weights for the operational satellite, nine estimates were made for each of two example configurations based on nominal and extreme values of solar array area and subsystem unit weights. Estimates for the column/ cable configuration are given in tables IV-A-5-1, -2, and -3 and for the truss configuration in tables IV-A-5-4, -5, and -6. The column/cable configuration which has been used for estimating purposes is illustrated in figure IV-A-4-1. Dimensions for the three overall efficiencies of section IV-A-2 are as follows: Dimensions for the truss configuration (figure IV-A-4-13) are:
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