• 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