NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
A thin-ply composite with embedded metallic mesh for a spaceborne antennaThis study presents a technique developed for embedding a conductive metallic mesh into the layup of thin-ply carbon fiber reinforced polymer (CFRP) composite material. Thermal cycling and subsequent mechanical testing on fabricated samples has been used to evaluate thin-ply composites as a crack mitigation technique. Furthermore, the construction of thin-ply
CFRP composite tubes has been demonstrated for both straight segments and curved segments utilizing a novel sacrificial ceramic molding method. These prototypes represent the building blocks for a 1 m scale radiating element and are the first test articles for the evaluation of thin-ply CFRP composites with an embedded metallic mesh. The successful
implementation of a CFRP composite with an embedded metallic mesh would enable ultra-lightweight conductive structures for future applications, such as antennas, requiring survival in cryogenic temperatures.
Document ID
20210009141
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
Authors
Sakovsky, Maria
Mihaly, Jonathan
Date Acquired
March 2, 2019
Publication Date
March 2, 2019
Publication Information
Publisher: Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2019
Distribution Limits
Public
Copyright
Other
Technical Review

Available Downloads

There are no available downloads for this record.
No Preview Available