An Investigation of Plume Rise from Titan IV Rocket Launches

Abstract

Space launches at Cape Canaveral Air Station (CCAS) and Vandenberg Air Force Base (vAFB) produce exhaust ground clouds from the solid rocket boosters and liquid hypergolic fuels containing several toxic substances. In order to estimate the health effects that would be imposed upon the public by scheduled launches, range safety officials rely on the Rocket Exhaust Effluent Diffusion Model to predict ground level concentrations of these substances. A drawback to the REEDM is its underprediction of the initial ground clouds stabilization height. This underprediction causes an overprediction of the ground level toxic substance concentrations. This thesis focused on increasing the accuracy of the clouds stabilization height. Therefore, a model was developed incorporating conservation principles of volume, momentum, and buoyancy to predict stabilization height values. As part of the model a predictive function for the coefficient of entrainment was developed based on meteorological conditions. This rate of entrainment is a critical factor in accurately predicting the rise behavior of ground exhaust clouds.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1997
Accession Number
ADA334357

Entities

People

  • Joseph D. Brands

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Biomedical
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Personnel
  • Algorithms
  • Atmospheric Motion
  • Buoyancy
  • Environment
  • Equations
  • Meteorological Data
  • Meteorological Phenomena
  • Meteorology
  • Military Personnel
  • Predictive Modeling
  • Rocket Exhaust
  • Statistical Analysis
  • Thermodynamics
  • Wind
  • Wind Shear

Fields of Study

  • Environmental science

Readers

  • Computational Modeling and Simulation
  • Ocean-Atmosphere Mesoscale Modeling, Data Assimilation, and Flux Boundary Layers
  • Rocket Propulsion.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster