Deployable Carbon-Fiber-Reinforced Polymer Boom with Bi-stability

被引：1
|
作者：
Kim, Sang Ki [1 ]
Kang, Jae Young [1 ]
机构：
[1] Inha Univ, Dept Mech Engn, Incheon, South Korea
来源：
TRANSACTIONS OF THE KOREAN SOCIETY OF MECHANICAL ENGINEERS A | 2021年 / 45卷 / 06期
关键词：
Deployable Structure; CFRP; Bi-stability; DYNAMIC-ANALYSIS; COMPOSITE;
D O I：
10.3795/KSME-A.2021.45.6.465
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
A carbon-fiber-reinforced polymer boom can be used for the frame of solar sail spacecraft. The boom needs to be coiled to package it before deployment in space. Design of the packaging and deployment configuration requires estimating the coiled diameter of the boom before it is manufactured. In this study, the coiled diameter under packaging is numerically calculated and it is validated by experiment.
引用
收藏
页码：465 / 471
页数：7
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