HCI in Rocket Exhaust Clouds: Atmospheric Dispersion,Acid Aerosol Characteristics,and Acid Rain Deposition

NASA is examining Space Shuttle launch impacts. Solid rocket exhaust includes ?60 tons HCL and ?87 tons alumina particles emitted below 2.5 km, of which 50-80% forms an altitude stabilized exhaust cloud (EC). Several 60% smaller Titan-Ill EC were sampled by aircraft for this study. Three distinct features are presented: (a) An analysis of HCL (gaseous plus aqueous) data traces. Total range of peak HCL was 25-0.5 ppm (3-300 min) for 8 EC. Power-law decays of peak HCL applied. Calculated HCL dispersions for 7 standard meteorologies are also shown, (b) An analysis of simultaneous HCL (g), HCL (g + aq) data for 2 EC. Vapor-liquid HCL/H₂O equilibria were calculated for a flat surface aqueous aerosol. HCL partitioning varied with EC dilution and H₂O content. HCL (aq) and aqueous mass fraction maximized early at >3 molal and >0.1 mg/g air. Calculated H₂O (g + aq) compared favorably with independent EC measurements, (c) An analysis of wet deposition after EC interception at ?30 min by a convective storm. A 28 km² acid chloride (1 < pH < 3) footprint was defined. In conclusion, (a) HCL dispersion in large EC tends to follow power-law decay, but HCL concentration may vary widely (100 times after 1 h) with meteorology, (b) HCL (g/aq) and H₂O (g/aq) partitioning is consistent with equilibrated acid aerosol compositions, and (c) localized deposition of highly acidic rain may occur sometimes.