It is shown that the radial shock of the satellite-rocket separation interface increases with the increase of the pre-tightening force of clamp band.
分析结果表明，分离面径向冲击随着包带预紧力增加而增大；
It is shown that the radial shock of the satellite-rocket separation interface increases with the increase of the pre-tightening force of clamp band.
分析结果表明，分离面径向冲击随着包带预紧力增加而增大；
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