A Preliminary Study of the Feasibility of Using a Pressurized Tube for the Soft Recovery of a Five Inch Projectile

Abstract

The report presents the results of a preliminary study of the possibility of using a pressurized tube to recover a standard five inch projectile with projectile decelerations no greater than 10% of the maximum in- bore acceleration. Computer calculations using both a simplified dynamics model and a one-dimensional Lagrangian hydrocode have been performed for a variety of recovery tube gases, initial pressures and tube lengths. Calculations were also made for tubes vented by blowing plugs out of the ends. Results of the calculations indicate that an initial pressurization of five to seven atmospheres is required to stop the projectile within the 10% limitation if a dense gas such as sulfur hexafluoride or Freon 12 is used. The required tube length is approximately 300 feet.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1973
Accession Number
AD0772523

Entities

People

  • L. P. Anderson Jr.

Organizations

  • Naval Surface Warfare Center Dahlgren Division

Tags

DTIC Thesaurus Topics

  • Atmospheres
  • Computer Programs
  • Computers
  • Deceleration
  • Dense Gases
  • Differential Equations
  • Equations
  • Gases
  • Hydrocodes
  • Partial Differential Equations
  • Physical Properties
  • Projectiles
  • Recovery
  • Shock Waves
  • Specific Heat
  • Test And Evaluation
  • Weapons

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Explosive Engineering.