Deployment shock attenuation of a solar array tape hinge by means of the Martensite detwinning of NiTi Shape Memory Alloy

被引:7
|
作者
Lee, Chang-Ho [1 ]
Jeong, Ju-Won [2 ]
Kim, Young-Jin [3 ]
Lee, Jung-Ju [2 ]
机构
[1] Korea Aerosp Res Inst, Daejeon 34133, South Korea
[2] Korea Adv Inst Sci & Technol, Dept Mech Engn, Daejeon 34141, South Korea
[3] Def Agcy Technol & Qual, Sacheon Reg Ctr, Dongjin Ro 420, Jinju 660031, Gyeongsangnam D, South Korea
来源
REVIEW OF SCIENTIFIC INSTRUMENTS | 2016年 / 87卷 / 03期
关键词
CONSTITUTIVE MODEL; BEHAVIOR;
D O I
10.1063/1.4943073
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
This paper presents a new tape hinge for attenuating the deployment shock of a satellite solar array. This hinge uses the Martensite detwinning of Shape Memory Alloy (SMA). To attenuate the deployment shock, a NiTi SMA strip is assembled between two curved steel strips. The attenuation performance of the hinge is analyzed using a SMA detwinning constitutive equation. A prototype of the hinge is manufactured and its characteristics are measured in a bending test and in a deployment test. Finally, the deployment performance of the prototype hinge is investigated on a satellite model. It is shown that the new SMA damped tape hinge can effectively minimize the deployment shock and dynamic perturbation while also maintaining suitable deployment performance. (C) 2016 AIP Publishing LLC.
引用
收藏
页数:9
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