Title:
ロケット結合リング及び宇宙機
Document Type and Number:
Japanese Patent JP6559519
Kind Code:
B2
Abstract:
PROBLEM TO BE SOLVED: To provide a rocket coupling ring having a structure that suppresses loads applied to a spacecraft at the time of launching.SOLUTION: A rocket coupling ring 100 is mounted to a spacecraft body in order to couple the spacecraft body to a rocket. The rocket coupling ring 100 includes: an annular ring body 10; multiple protruding parts 21 disposed so as to respectively protrude upward from a top edge of the ring body 10; and multiple support parts 22 disposed on a top edge part of each of the multiple protruding parts 21 in order to support the spacecraft body. Specifically, the support part 22 is disposed on the top edge part of a corresponding protruding part 21. The multiple protruding parts 21 are intermittently arranged in a circumferential direction of the ring body 10, and are respectively elastically deformable in a radial direction of the ring body 10.SELECTED DRAWING: Figure 2
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Inventors:
Kazuyuki Nakamura
Application Number:
JP2015184996A
Publication Date:
August 14, 2019
Filing Date:
September 18, 2015
Export Citation:
Assignee:
Technosolver Co., Ltd.
International Classes:
B64G1/64
Domestic Patent References:
JP8261279A |
Foreign References:
US20040011942 | ||||
DE102008046149B3 |
Attorney, Agent or Firm:
Shunsuke Umeda