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acute contact angles adhesion of deposited Aeronautics and Space Beam voltage bond layer followed Candidate Graphite-Fiber/Coating Combinations carbon fiber coating on graphite coatings were resistance collection of information Composite Candidate Graphite-Fiber/Coating composites of graphite context of creating copper adhesion copper coverage copper matrix copper on graphite copper ref Copper-clad fibers copper/titanium fiber copper/tungsten delaminate direct-current power supply edge of Image electron micrographs Fiber bundle fiber samples Fiber surface wetting fiber temperature fibers were heated films at elevated followed by copper graphite fibers heating fig Heating of Composite high contact angle Individual fibers interfacial bond layer Lewis Research Center long-focal-length optical pyrometer melting temperature metal and fiber NASA National Aeronautics nonwetting behavior Ohmic Heating pure copper relatively quick REPORT NUMBER resistance heated SECURITY CLASSIFICATION self-heating Space Administration SPONSORING/MONITORING AGENCY test the adhesion thermocouple thin titanium bond titanium bond layer tungsten bond layer vacuum to test Visibly patchy wetting or nonwetting X-ray spectrometer