Trajectory Predictions for a 75 mm Solid Fuel Ramjet Tubular Projectile

Abstract

The AFAPL ramjet design analysis code was modified to predict a point mass trajectory for a 75 mm solid fuel ramjet tubular projectile. Projectile velocity was found sensitive to the combustion efficiency relation assumed.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1981
Accession Number
ADA105551

Entities

People

  • Carl W. Nelson

Organizations

  • Ballistic Research Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Temperature
  • Chambers
  • Chemical Engineering
  • Combustion
  • Combustion Chambers
  • Efficiency
  • Engineering
  • Fuels
  • Mechanical Engineering
  • Military Research
  • Munitions
  • Projectiles
  • Sea Level
  • Solid Fuels
  • Standards
  • Trajectories
  • Weapons

Fields of Study

  • Physics

Readers

  • Internal Combustion Engine (ICE) Technology.
  • Regression Analysis.
  • ballistics.