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Diffusion algorithms and data reduction routine for onsite launch predictions for the transport of Titan 3 C exhaust effluentsThe 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.
Document ID
19750005994
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Stephens, J. B.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hamilton, P. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1974
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TN-D-7862
Report Number: NASA-TN-D-7862
Accession Number
75N14066
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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