DocumentCode
1791780
Title
SMA-based space release device for solar panels deployment
Author
Liu Gangfeng ; Yan Jihong ; Yang Chen ; Zhao Jie ; Zhao Ying
Author_Institution
State Key Lab. of Robotic & Syst., Harbin Inst. of Technol., Harbin, China
fYear
2014
fDate
3-6 Aug. 2014
Firstpage
27
Lastpage
31
Abstract
Most of separating operations for solar panels have been achieved by utilizing explosive bolt nowadays. However, with the development of space technology, especially when new generations of small satellites start to emerge, traditional pyrotechnical products cannot provide spacecrafts with satisfied performance, since the fierce shock and contamination are not avoidable. Thus, developing novel types of non-pyrotechnical actuators has become the research focus for release mechanism. In this paper, we propose to adopt the memory effect of the shape memory alloy (SMA) for developing release devices. Brinson theory has been chosen as the theoretical foundation of performance analysis. This new type of mechanism mitigates the problem of shock and contamination, meanwhile possessing several excellent advantages such as compact volume, quick response, outstanding synchronism and reusability.
Keywords
shape memory effects; solar cells; Brinson theory; SMA-based space release device; compact volume; memory effect; performance analysis; quick response; reusability; shape memory alloy; solar panels deployment; synchronism; Actuators; Force; Mathematical model; Shape memory alloys; Space vehicles; Springs; Wires; SMA-spring actuator; constitutive model; deployment simulation; solar panels; space release mechanism;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation (ICMA), 2014 IEEE International Conference on
Conference_Location
Tianjin
Print_ISBN
978-1-4799-3978-7
Type
conf
DOI
10.1109/ICMA.2014.6885666
Filename
6885666
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