Diffusion algorithms and data reduction routine for onsite launch predictions for the transport of Titan 3 C exhaust effluents

Details Diffusion algorithms and data reduction routine for onsite launch predictions for the transport of Titan 3 C exhaust effluents Diffusion algorithms and data reduction routine for onsite launch predictions for the transport of Titan 3 C exhaust effluents

Dec 1974

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1974stin...7514066s&link_type=abstract

Unknown

Physics

Algorithms, Data Reduction, Exhaust Gases, Titan 3 Launch Vehicle, Aerospace Environments, Dispersions, Fluid Mechanics, Kinematics, Thermodynamics

Scientific paper

The NASA/MSFC multilayer diffusion algorithms have been specialized for the prediction of the surface impact for the dispersive transport of the exhaust effluents from the launch of a Titan 3 vehicle. This specialization permits these transport predictions to be made at the launch range in real time so that the effluent monitoring teams can optimize their monitoring grids. Basically, the data reduction routine requires just the meteorology profiles for the thermodynamics and kinematics of the atmosphere as an input. These profiles are graphed along with the resulting exhaust cloud rise history, the center line concentrations and dosages, and the hydrogen chloride isopleths.

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