《Tab.3 Fairing Dimensions 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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For the small-sat specific launchers，the available space for small satellites is determined by design of payload fairing envelop.Four dimensions of the fairing envelop，which are including cylinder diameter，cylinder length，cone length and cone tip diameter（See Fig.1），are chosen to make comparison analyses to these fairings（See Tab.3）.