• DocumentCode
    2567596
  • Title

    Active polymers for space applications

  • Author

    Jenkins, C.H. ; Vinogradov, A.M.

  • Author_Institution
    Dept. of Mech. Eng., South Dakota Sch. of Mines & Technol., Rapid City, SD, USA
  • Volume
    7
  • fYear
    2000
  • fDate
    2000
  • Firstpage
    415
  • Abstract
    Membrane/inflatable structures for space applications holds great promise. Their reduced launch mass and stowed volume suggest the possibility of large aperture antenna and reflectors for increased resolution, and solar sails and shades that can span great distances. However, their extreme flexibility provides for significant engineering challenges. Control of their shape will require sensors and actuators that are complementary with the lightweight and flexible nature of these structures. Active polymers such as PVDF fit this role well, and we begin this paper with a review of the mechanical properties of this material. Then we provide an analytical example that shows how PVDF might be applied to improve the shape of a doubly-curved membrane reflector
  • Keywords
    actuators; membranes; polymers; reflector antennas; solar absorber-convertors; space vehicles; PVDF; active polymers; actuators; doubly-curved membrane reflector; inflatable structures; large aperture antenna; launch mass; mechanical properties; solar sails; solar shades; space applications; stowed volume; Biomembranes; Mechanical factors; Mechanical sensors; Optical surface waves; Packaging; Piezoelectric materials; Polymers; Radar applications; Shape control; Space technology;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2000 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-5846-5
  • Type

    conf

  • DOI
    10.1109/AERO.2000.879308
  • Filename
    879308