发明名称 INTER-STAGE COUPLING SEPARATION DEVICE FOR ROCKET
摘要 PROBLEM TO BE SOLVED: To separate an inter-stage part of a rocket without requiring a band clamping mechanism or a band holding mechanism of complicated construction. SOLUTION: The ends of clamp bands 11 which hold clamps 12 separably engaging each other across an inter-stage part 4 of a rocket 1 are connected to form a clamp ring 11A. An extension mechanism 20 for keeping a fastened state where the clamp 12 is engaged with the inter-stage part 4 up to the state where the inter-stage part 4 of the rocket 1 is separated, and for elongating the peripheral length of the clamp ring 11A to separate the clamp 12 from the inter-stage part 4 at the stage the inter-section part 4 of the rocket 1 is separated, is provided at the clamp ring 11A.
申请公布号 JP2000006899(A) 申请公布日期 2000.01.11
申请号 JP19980171685 申请日期 1998.06.18
申请人 NISSAN MOTOR CO LTD 发明人 YAGI KAZUHIRO
分类号 F42B15/36;B64G1/64;(IPC1-7):B64G1/64 主分类号 F42B15/36
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