《Tab.4 Launch Volumes and Launch Densities of Small-sat Specific Launchers》

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《国际市场微小卫星发射服务定位分析（英文）》

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According to the dimensions from Tab.3，parameters are calculated and listed（see Tab.4），in which the launch volume is the sum of cylinder volume and cone effective volume of the fairing envelop.Because the conventional low utilization rate of the cone volume，the effective volume of the cone is put forward here and defined as the3/4 of cone volume.The launch density of a launcher is also put forward to evaluate the spaciousness where the satellites are serviced，which is defined by a ratio of the launch capacity to the launch volume.Besides，in order to compare the shapes of fairings，the total length-diameter ratios are calculated.