Simulating Oxidation of Carbon Surfaces by Atomic Oxygen Coupled with a Finite Rate Oxidation Model

2022 ◽  
Author(s):  
Kaan K. Kirmanoglu ◽  
Nicholas A. Anderson ◽  
Francesco Panerai ◽  
Kelly A. Stephani ◽  
Joseph C. Ferguson ◽  
...  
AIAA Journal ◽  
2017 ◽  
Vol 55 (5) ◽  
pp. 1644-1658 ◽  
Author(s):  
Savio Poovathingal ◽  
Thomas E. Schwartzentruber ◽  
Vanessa J. Murray ◽  
Timothy K. Minton ◽  
Graham V. Candler

Author(s):  
Savio J. Poovathingal ◽  
Thomas E. Schwartzentruber ◽  
Vanessa Murray ◽  
Timothy K. Minton ◽  
Graham V. Candler

Carbon ◽  
2018 ◽  
Vol 137 ◽  
pp. 313-332 ◽  
Author(s):  
Krishnan Swaminathan-Gopalan ◽  
Arnaud Borner ◽  
Vanessa J. Murray ◽  
Savio Poovathingal ◽  
Timothy K. Minton ◽  
...  

1989 ◽  
Vol 39 (1-4) ◽  
pp. 89-102 ◽  
Author(s):  
J.M. Delarios ◽  
C.R. Helms ◽  
D.B. Kao ◽  
B.E. Deal

2013 ◽  
Vol 28 (8) ◽  
pp. 853-858 ◽  
Author(s):  
Cong TIAN ◽  
Lai-Fei CHENG ◽  
Xin-Gang LUAN

2000 ◽  
Vol 12 (1) ◽  
pp. 43-52 ◽  
Author(s):  
John W Connell

Thin films of phenylphosphine oxide-containing polymers were exposed to low Earth orbit aboard a space shuttle flight (STS-85) as part of flight experiment designated Evaluation of Space Environment and Effects on Materials (ESEM). This flight experiment was a cooperative effort between the NASA Langley Research Center (LaRC) and the National Space Development Agency of Japan (NASDA). The thin-film samples described herein were part of an atomic oxygen exposure (AOE) experiment and were exposed to primarily atomic oxygen (∼1×1019 atoms cm−2). The thin-film samples consisted of three phosphine oxide-containing polymers (arylene ether, benzimidazole and imide). Based on post-flight analyses using atomic force microscopy, x-ray photo-electron spectroscopy and weight loss data, it was found that the exposure of these materials to atomic oxygen (AO) produces a phosphorus oxide layer on the surface of the samples. Earlier work has shown that this layer provides a barrier towards further attack by AO. Consequently, these materials do not exhibit linear erosion rates which is in contrast with most organic polymers. Qualitatively, the results obtained from these analyses compare favourably with those obtained from samples exposed to AO and/or an oxygen plasma in ground-based exposure experiments. The results of the low Earth orbit AO exposure on these materials will be compared with those of ground-based exposure to AO.


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