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Electrostatic Discharge Testing of Carbon Composite Solar Array Panels for the Europa Mission to JupiterCarbon composite solar array panel coupons similar to those considered for use on the planned NASA Europa Mission were exposed to energetic electrons to observe the size and rate of electrostatic discharge production. The discharge size and rate were found to be primarily dependent on the quantity of dielectric binder pooled on the surface of the sample. Cooling the samples to cryogenic temperatures increased the size of discharges but an end of mission radiation dose had only minimal effects. Samples were composed of M55J carbon composite impregnated with an RS3 binder. Additional samples tested included a co-cured Kapton surface.
Document ID
20190025588
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Green, Nelson W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Dawson, Stephen F.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
June 3, 2019
Publication Date
April 4, 2016
Subject Category
Composite Materials
Report/Patent Number
JPL-CL-16-1974
Meeting Information
Meeting: Spacecraft Charging Technology Conference
Location: Noordwijik
Country: Netherlands
Start Date: April 4, 2016
End Date: April 8, 2016
Sponsors: European Space Agency. European Space Research and Technology Center, ESTEC
Distribution Limits
Public
Copyright
Other

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