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

Author:

Lee Chang-Ho12,Jeong Ju-Won2,Kim Young-Jin3,Lee Jung-Ju2

Affiliation:

1. Korea Aerospace Research Institute, Daejeon 34133, South Korea

2. Department of Mechanical Engineering, Korea Advanced Institute of Science and Technology, Daejeon 34141, South Korea

3. Sacheon Regional Center, Defense Agency for Technology and Quality, Dongjin-ro 420, Jinju 660-031, Gyeongsangnam-do, South Korea

Publisher

AIP Publishing

Subject

Instrumentation

Reference20 articles.

1. H. Arends et al., “The MIDAS experiment for the Rosetta mission,” in 9th European Space Mechanisms and Tribology Symposium, Liège, 2001.

2. Experimental-Analytical Qualification of a Piezoelectric Mechanism for a Critical Space Application

3. C. Menon et al., “Concept design of novel bio-inspired distributed actuators for space applications,” IAC-06–D1.1.06 (2006).

4. N. Nova et al., “New development mechanisms based on SMA technology for space applications,” in 15th European Space Mechanisms and Tribology Symposium, Noordwijk, 2013.

5. Passive and smart mechanical behaviour of auxetic open cell PU foams

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