Effective emissivities of high-temperature fiber composites are calculated for several external edge surface structuressrandomly overlapping, parallel cylinders of radius a protruding out a distance δ from the composite matrix, with central axes either perpendicular to or into the direction of the composite external edge. Firstorder multiple scattering reciprocal bounds provide effective emissivity values, usually within an error of 10% or less; e.g., for carbon-carbon composites with a fiber-matrix emissivity of ε s ) 0.8 and a fiber fraction of 30 vol %, the maximum error bound is 4%-5%. The fundamental behavior of the effective emissivity, as a function of protrusion depth, is examined, and significant deep-bed, blackbody radiative effects are observed, even at modest model protrusions. A maximum value for the fiber composite effective emissivity at an optimum porosity is found for any given ratio of protrusion length to fiber radius (δ/a) and fiber-matrix emissivity (ε s ); e.g., for a perpendicular protrusion with δ/a ) 3 and ε s ) 0.5, a maximum effective emissivity enhancement of 27% is found at Φ ) 0.6, and for fibers protruding parallel to the edge with δ/a ) 3 and ε s ) 0.5, a maximum enhancement of 21% is observed at Φ ) 0.6. Model equation results agree with the measured effective emissivity values of carbon-carbon brake composites.