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Adsorption and chemical reaction of gaseous mixtures of hydrogen chloride and water on aluminum oxide and application to solid-propellant rocket exhaust cloudsHydrogen chloride (HCl) and aluminum oxide (Al2O3) are major exhaust products of solid rocket motors (SRM). Samples of calcination-produced alumina were exposed to continuously flowing mixtures of gaseous HCl/H2O in nitrogen. Transient sorption rates, as well as maximum sorptive capacities, were found to be largely controlled by specific surface area for samples of alpha, theta, and gamma alumina. Sorption rates for small samples were characterized linearly with an empirical relationship that accounted for specific area and logarithmic time. Chemisorption occurred on all aluminas studied and appeared to form from the sorption of about a 2/5 HCl-to-H2O mole ratio. The chemisorbed phase was predominantly water soluble, yielding chloride/aluminum III ion mole ratios of about 3.3/1 suggestive of dissolved surface chlorides and/or oxychlorides. Isopiestic experiments in hydrochloric acid indicated that dissolution of alumina led to an increase in water-vapor pressure. Dissolution in aqueous SRM acid aerosol droplets, therefore, might be expected to promote evaporation.
Document ID
19780014245
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Cofer, W. R., III
(NASA Langley Research Center Hampton, VA, United States)
Pellett, G. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1978
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
NASA-TP-1105
L-11800
Accession Number
78N22188
Funding Number(s)
PROJECT: RTOP 506-21-30-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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