DocumentCode
2109210
Title
Novel micro electro mechanical systems (MEMS) packaging for the skin of the satellite
Author
Darrin, M.A. ; Osiander, Robert ; Lehtonen, John ; Farrar, Dawnielle ; Douglas, Donya ; Swanson, Ted
Author_Institution
Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD, USA
Volume
4
fYear
2004
fDate
13-13 March 2004
Firstpage
2486
Abstract
This paper includes a discussion of the novel packaging techniques that are needed to place MEMS based thermal control devices on the skin of various satellites, eliminating the concern associated with potential particulates from integration and test or the launch environment. Protection of this MEMS based thermal device is achieved using a novel polymer that is both IR transmissive and electrically conductive. This polymer was originally developed and qualified for space flight application by NASA at the Langley Research Center. The polymer material, commercially known as CP1, is coated with a thin layer of ITO and sandwiched between two window-like frames. The packaging of the MEMS based radiator assembly offers the benefits of micro-scale devices in a chip on board fashion, with the level of protection generally found in packaged parts.
Keywords
aerospace control; chip-on-board packaging; conducting polymers; micromechanical devices; optical polymers; space vehicle electronics; thermal management (packaging); thermal variables control; CP1 polymer; IR transmissive polymer; ITO layer; Langley Research Center; MEMS based radiator assembly packaging; MEMS based thermal device protection; NASA; chip on board package; electrical conductive polymer; microelectromechanical systems packaging; microscale devices; satellite skin; space flight application; thermal control devices; window-like frames; Mechanical systems; Micromechanical devices; NASA; Packaging; Polymers; Protection; Satellites; Skin; Testing; Thermal conductivity;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2004. Proceedings. 2004 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
0-7803-8155-6
Type
conf
DOI
10.1109/AERO.2004.1368043
Filename
1368043
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