PREDICTIONS OF THE TERMINAL ALTITUDE AND SIZE OF LARGE BUOYANT CLOUDS GENERATED BY ROCKET LAUNCHES.

Abstract

Motion pictures of launches of Titan III solid rocket motors were used, in conjunction with conservation equations and knowledge of rocket plume properties, to determine the initial temperature and mass of the large cloud that is generated during these launches. These initial conditions were applied to a mathematical model which accounted for buoyancy, drag, and entrainment. The model predicted the radius, altitude, temperature, and mass of the cloud as a function of time. The results showed fair agreement with size and altitude data extracted from the movies. This methodology was applied with limited success to smaller scale rocket clouds generated at test stands. The model was also used to predict the behavior of large exhaust clouds under various external temperature profiles. There is some experimental evidence that the model correctly accounts for unstable profiles, and the predictions of cloud rise during inversion conditions agree with what intuition would predict. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 01, 1970
Accession Number
AD0707110

Entities

People

  • William S. Hart

Organizations

  • The Aerospace Corporation

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Agreements
  • Altitude
  • Buoyancy
  • Entrainment
  • Equations
  • Inversion
  • Mathematical Models
  • Models
  • Motion Pictures
  • Rocket Engines
  • Rockets
  • Terminals
  • Test Stands

Readers

  • Atmospheric Remote Sensing.
  • Combustion and Flow Dynamics.
  • Rocket Propulsion.