NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Electrical Breakdown of Anodized Structures in a Low Earth Orbital EnvironmentalA comprehensive set of investigations involving arcing on a negatively biased anodized aluminum plate immersed in a low density argon plasma at low pressures (P(sub O), 7.5 x 10(exp -5) Torr) have been performed. These arcing experiments were designed to simulate electrical breakdown of anodized coatings in a Low Earth Orbital (LEO) environment. When electrical breakdown of an anodized layer occurs, an arc strikes, and there is a sudden flux of electrons accelerated into the ambient plasma. This event is directly followed by ejection of a quasi-neutral plasma cloud consisting of ejected material blown out of the anodized layer. Statistical analysis of plasma cloud expansion velocities have yielded a mean propagation velocity, v = (19.4 +/- 3.5) km/s. As the plasma cloud expands into the ambient plasma, energy in the form of electrical noise is generated. The radiated electromagnetic noise is detected by means of an insulated antenna immersed in the ambient plasma. The purpose of the investigations is (1) to observe and record the electromagnetic radiation spectrum resulting from the arcing process. (2) Make estimates of the travel time of the quasi-neutral plasma cloud based on fluctuations to several Langmuir probes mounted in the ambient plasma. (3) To study induced arcing between two anodized aluminum structures in close proximity.
Document ID
19990052584
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Galofaro, J. T.
(NASA Glenn Research Center Cleveland, OH United States)
Doreswamy, C. V.
(Tuskegee Inst. AL United States)
Vayner, B. V.
(Ohio Aerospace Inst. Cleveland, OH United States)
Snyder, D. B.
(NASA Glenn Research Center Cleveland, OH United States)
Ferguson, D. C.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1999
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:209044
E-11574
NASA/TM-1999-209044
Funding Number(s)
PROJECT: RTOP 632-1A-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available