DocumentCode :
356907
Title :
Spacecraft charging effects on anodized aluminum surfaces
Author :
Hillard, G.B. ; Vagner, B.
Author_Institution :
NASA Glen Res. Center, Cleveland, OH, USA
Volume :
1
fYear :
2000
fDate :
2000
Firstpage :
63
Abstract :
Because of a number of key properties, there is increased interest in using anodized aluminum on external spacecraft surfaces. Originally used by the space station program because aluminum is cheap and easy to anodize, it attracted attention because its optical properties, especially absorptivity and emissivity, can be tailored to produce a surface having excellent thermal control properties. Furthermore, since it is an oxide and is almost impervious to atomic oxygen (AO) it is ideal for use in low Earth orbit (LEO) where AO attack is a major design issue. In addition to these traditional uses of the material, the recent introduction of high-voltage space power systems has caused designers to take note of the excellent insulating properties of this material. As a result, both laboratory work as well as limited space testing has been performed. The authors show a typical sample from high voltage arc testing as well as a flight sample from the Solar Array module Plasma Interactions Experiment (SAMPIE). They believe their findings to apply generally to this material as they assess its value as a high voltage insulator in space
Keywords :
aerospace testing; aluminium; anodisation; insulating materials; space vehicle power plants; spacecraft charging; Al; Solar Array module Plasma Interactions Experiment; anodized aluminum surfaces; atomic oxygen; external spacecraft surfaces; high voltage arc testing; high voltage insulator; high-voltage space power systems; insulating properties; low Earth orbit; space testing; spacecraft charging effects; thermal control properties; Aerospace materials; Aluminum; Atom optics; Insulation; Low earth orbit satellites; Space stations; Space vehicles; Surface charging; Testing; Voltage;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Energy Conversion Engineering Conference and Exhibit, 2000. (IECEC) 35th Intersociety
Conference_Location :
Las Vegas, NV
Print_ISBN :
1-56347-375-5
Type :
conf
DOI :
10.1109/IECEC.2000.870628
Filename :
870628
Link To Document :
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