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
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