TY - GEN
T1 - High-temperature oxidation of graphite under non-thermal oxygen plasma
AU - Anderson, Nicholas A.
AU - Bhattacharya, Souvik
AU - Kirmanoglu, Kaan
AU - Stephani, Kelly
AU - Elliott, Gregory S.
AU - Sankaran, R. Mohan
AU - Panerai, Francesco
N1 - Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2022
Y1 - 2022
N2 - Experiments to measure the oxidation rates of carbon by molecular and atomic oxygen were conducted using a non-thermal, radio frequency generated plasma exposed to a resis-tively heated graphite rod at surface temperatures between 773 and 2073 K. The temperature dependence of oxidation behavior was obtained for pure O2 and for a mixture of O2 and O atoms produced by the plasma. Oxygen atom flux to the graphite samples was characterized based on etching rates of reference polyimide films. Mass loss and exposure time of the graphite samples were measured at different test conditions to calculate oxidation rates. Mass spectrometry was used to identify the chemical species present in the oxidation products. Experiments were carried out at a pressure of 0.33 kPa which provided carbon oxidation results relevant to atmospheric entry conditions and which will be used to inform Arrhenius rate equations for gas-surface interaction computational models.
AB - Experiments to measure the oxidation rates of carbon by molecular and atomic oxygen were conducted using a non-thermal, radio frequency generated plasma exposed to a resis-tively heated graphite rod at surface temperatures between 773 and 2073 K. The temperature dependence of oxidation behavior was obtained for pure O2 and for a mixture of O2 and O atoms produced by the plasma. Oxygen atom flux to the graphite samples was characterized based on etching rates of reference polyimide films. Mass loss and exposure time of the graphite samples were measured at different test conditions to calculate oxidation rates. Mass spectrometry was used to identify the chemical species present in the oxidation products. Experiments were carried out at a pressure of 0.33 kPa which provided carbon oxidation results relevant to atmospheric entry conditions and which will be used to inform Arrhenius rate equations for gas-surface interaction computational models.
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U2 - 10.2514/6.2022-0114
DO - 10.2514/6.2022-0114
M3 - Conference contribution
AN - SCOPUS:85122700573
SN - 9781624106316
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
BT - AIAA SciTech Forum 2022
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Y2 - 3 January 2022 through 7 January 2022
ER -