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An Investigation of International Space Station Trace Contaminant Oxidation Catalyst Poisoning
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English
Abstract
The Trace Contaminant Control System (TCCS) removes most hazardous contaminants from the space station atmosphere using a carbon bed, but some must be destroyed in a high temperature catalytic oxidizer. While the oxidizer is protected from catalyst poisons by the carbon bed, if contaminant loads are greater than anticipated, the catalyst may be exposed to a variety of poisons. Thus, we studied the effect of halocarbons, sulfides and nitrogen compounds on the catalytic activity and the products produced. We found that even if poisoning occurs, the catalyst will recover, and will not produce toxic partial oxidation products.
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Authors
Citation
Wright, J., Chen, B., Wang, C., Perry, J. et al., "An Investigation of International Space Station Trace Contaminant Oxidation Catalyst Poisoning," SAE Technical Paper 961517, 1996, https://doi.org/10.4271/961517.Also In
References
- Leban, M.I. Kawasaki E.H. Conine G.P. 1991 “Performance Characterization of Activated Carbon and Oxidation Catalyst for Gaseous Trace Contaminant Control,” SAE 911548 21st International Conference on Environmental Systems San Francisco, CA July 15-18
- Link, D.E., Jr. Angeli J.W. 1991 “A Gaseous Trace Contaminant Control System for the Space Station Freedom Environmental Control and Life Support System,” SAE 911452 21st International Conference on Environmental Systems San Francisco, CA July 15-18
- Perry, J.L. 1995 “Trace Chemical Contaminant Generation Rates for Spacecraft Contamination Control System Design,” NASA Technical Memorandum 108497
- Wright, J.D. Chen B. Wang C. 1996 “Trace Contaminant Oxidation Catalyst Poisoning Investigation,” Final report for NASA Contract NAS8-38250-15