Bipropellant Engine Plume Contamination Program. Volume III. Performance Predictions for the AJ10-181 Bi-Propellant Rocket Engine Using the CONTAM/TCC code

Abstract

A plume contamination test conducted in the AEDC Aerospace Chamber (10V) with the Aerojet AJ10-181 5-lb-thrust bipropellant engine provided data for comparison with the CONTAM computer program. The Plume Contamination Effects Prediction Program (CONTAM), developed by McDonnell Douglas under Air Force Rocket Propulsion Laboratory (AFRPL) sponsorship, comprises several component codes which describe the gas dynamics and chemistry. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1979
Accession Number
ADA074914

Entities

People

  • M. Kinslow
  • W. B. Stephenson

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Bipropellants
  • Chambers
  • Combustion
  • Combustion Chambers
  • Computational Science
  • Computer Programs
  • Engineering
  • Flow Rate
  • Ignition
  • Injectors
  • Jet Propulsion
  • Latent Heat
  • Propellants
  • Rocket Engines
  • Tennessee
  • United States

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Nuclear Civil Defense.
  • Rocket Propulsion.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster