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Diffusion algorithms and data reduction routine for onsite launch predictions for the transport of titan 3 c exhaust effluents
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hamilton, P. A. Stephens, J. B. |
| Copyright Year | 1974 |
| Description | 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. |
| File Size | 3019435 |
| Page Count | 88 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750005994 |
| Archival Resource Key | ark:/13960/t9n34mt3c |
| Language | English |
| Publisher Date | 1974-12-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Fluid Mechanics Thermodynamics Titan 3 Launch Vehicle Algorithms Aerospace Environments Exhaust Gases Kinematics Dispersions Data Reduction Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
