The behavior was investigated of graphite and several charring ablators in a variety of high-radiative heat-flux environments. A commercial-grade graphite and nine state-of-the-art charring ablators were subjected to various radiative environments produced by a CO2 laser and a carbon arc. Graphite was also tested in xenon-arc radiation. Heat-flux levels ranged from 10 to 47 MW/sq m. Tests were conducted in air, nitrogen, helium, and a CO2-N2 mixture which simulated the Venus atmosphere. The experimental results were compared with theoretical results obtained with a one-dimensional charring-ablator analysis and a two-dimensional subliming-ablator analysis. Neither the graphite nor the charring ablators showed significant differences in appea...
Hemispherical spectral emittance of ablation chars, carbon, and zirconia during atmospheric reentr
Eighteen material properties were measured on 45 different, commercially available, artificial graph...
Design and tests of graphite radiant heater for high heat flux source in spacecraft thermostructural...
The behavior of graphite and several charring ablators in a variety of high radiative heat flux envi...
Performance tests for ablative materials subjected to high intensity carbon dioxide laser radiatio
The stagnation-point ablation rates of a graphite, a carbon-carbon composite, and four carbon-phenol...
Ablation performance of glasslike carbons, pyrolytic graphite, and artificial graphite in stagnation...
Numerical simulations have been performed to study radiative and ablative processes experienced by a...
Eighteen material properties were measured on 45 different, commercially available, artificial graph...
In a number of areas the Army has need for high-0temperature, heat-shielding materials that retain s...
Tactical missions for laser weapons include a wide variety of targets, increasing the demands on the...
Ablation behavior of charring material in high velocity streams of arc heated air, nitrogen, and arg...
Interaction between material ablation products and simulated atmosphere entry heat studied in tests ...
Despite the prominence of carbon-based materials for use in thermal protection systems,much uncertai...
Energy transfer in pyrolysis product flow through char layer of nylon phenolic resin ablato
Hemispherical spectral emittance of ablation chars, carbon, and zirconia during atmospheric reentr
Eighteen material properties were measured on 45 different, commercially available, artificial graph...
Design and tests of graphite radiant heater for high heat flux source in spacecraft thermostructural...
The behavior of graphite and several charring ablators in a variety of high radiative heat flux envi...
Performance tests for ablative materials subjected to high intensity carbon dioxide laser radiatio
The stagnation-point ablation rates of a graphite, a carbon-carbon composite, and four carbon-phenol...
Ablation performance of glasslike carbons, pyrolytic graphite, and artificial graphite in stagnation...
Numerical simulations have been performed to study radiative and ablative processes experienced by a...
Eighteen material properties were measured on 45 different, commercially available, artificial graph...
In a number of areas the Army has need for high-0temperature, heat-shielding materials that retain s...
Tactical missions for laser weapons include a wide variety of targets, increasing the demands on the...
Ablation behavior of charring material in high velocity streams of arc heated air, nitrogen, and arg...
Interaction between material ablation products and simulated atmosphere entry heat studied in tests ...
Despite the prominence of carbon-based materials for use in thermal protection systems,much uncertai...
Energy transfer in pyrolysis product flow through char layer of nylon phenolic resin ablato
Hemispherical spectral emittance of ablation chars, carbon, and zirconia during atmospheric reentr
Eighteen material properties were measured on 45 different, commercially available, artificial graph...
Design and tests of graphite radiant heater for high heat flux source in spacecraft thermostructural...