Abstract
An important factor in the use of graphite in space applications is its rate of oxidation or ablation at high temperature in high flow environments during re-entry. This paper presents a study of the kinetics and mechanism of ablation of two types of graphite at temperatures of 1200° to 1332 °C in oxygen and air, at pressures of 5 and 9.5 torr, and at flow rates of 7.6 × 10 18 to 1.6 × 10 20 atoms of oxygen per second. A rate of ablation of 5.7 × 10 19 atoms of carbon per cm 2-sec was observed at an oxygen pressure of 9.5 torr and at 1332 °C. These fast ablation rates were fitted to a reaction mechanism based on the mobile adsorption of oxygen as the rate limiting step, with a heat of activation of 39,000 calories per mole. Comparison of the rate data with collision theory calculations showed 1.9% of the oxygen collisions resulted in reaction. Mass spectrometer analyses of the reaction products indicated carbon monoxide as the primary reaction product.
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