Catalytic combustion coupled with activated carbon and molecular sieve adsorbents is applicable to all areas of air and gas clean up ranging from high to low levels of pollutants and trace contaminants control in a spacecraft environment is of no exception. In this study we propose a combined activated charcoal and catalytic combustion system based on a 70 watt power input achieving 350°C, operating on a 6 hour per 24 hour day catalytic cycle with an actual flow of 10.6 l min-1 in a residual free volume of 60 m3. The catalysts are optimally sized for keeping the contaminants within a specified limits whilst paying particular attention to the following design parameters in descending order of priority power consumption, catalyst mass and catalyst volumeWe consider 2 conceptual catalytic systems namely: The catalysts are precious metals on single or mixed base oxides to give the sustained low temperature performance. One of the catalyst is an extruded monolith of 200 cells per square inch and the other is a washcoated honeycomb substrate (cordierite) of 600 cpsi. The ceramic monolith has some significant advantages over the granular type catalyst namely Low pressure drop Large geometric area Low coefficient of expansion Good thermal shock resistance Good vibration and crushing resistance The two recommended catalysts of different formulations are:Pt /Pd on extruded 200 cpsi titania monolithPt/Pd on tin IV oxide washcoated on 600 cpsi cordierite monolithThe Pt/TiO2 is a high destruction catalyst operating at high GHSV at low light off temperature. Our results show that it completely oxidises 300 ppm CH4 at 21000 h-1 in the temperature range 180-280°C. It oxidises 0.3% chloromethane (3000 ppmv) at GHSV of 21000 h-1 and 500°C. The combustion of halocarbons requires a post-charcoal filter to remove the haloacids formed. The versatility of Pt/TiO2 is shown in its ability to oxidise completely an aliphatic alcohol, an unsaturated aromatic, an aliphatic amine, and a straight chain aliphatic paraffin at 60000 h-1 in the temperature range 150-350°C with an inlet concentration of 500 ppmv.The Pt/Pd on Sn(IV)O2 is an ambient temperature catalyst and will oxidise H2 and CO at room temperature. Our results show that this catalyst oxidises 300 ppmv CO saturated with water vapour at an inlet temperature of 24°C and operating at 72000 h-1 with a residual of 8 ppmv CO. Our study is based on an assumed list of likely contaminants, their generation rate, and a maximum allowable concentration, thence we recommend catalyst size and operating conditions based on experimental catalysts performance.
A Catalytic Combustion System Coupled with Adsorbents for Air Clean Up in Sealed Spacecraft Environment
Sae Technical Papers
International Conference On Environmental Systems ; 2003
2003-07-07
Aufsatz (Konferenz)
Englisch
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