Experimental Hypervelocity Firings Using Stick and Granular Propellant Configurations

Abstract

The suitability of lumped-parameter interior ballistic models for prediction of the interior ballistic performance of very high velocity guns is limited by use of a predetermined pressure gradient which is superimposed on the solution to approximate the relationship between space-mean, breech and projectile base pressures. Even modern two-phase flow interior ballistic models, specifically formulated to address the hydrodynamics of the problem, have not been extensively exercised in this regime. Only recently have limited, large- caliber gun firings with realistic projectile masses been conducted to provide required data in this velocity regime. In this study, firings were conducted in a long 120-mm gun at propellant charge to projectile mass ratios (C/M) of about 3 to 6, yielding muzzle velocities in the 2 - 2.7 km/s range. The tube was instrumented with pressure gages at various locations along its length to provide data for comparison to predictions of various interior ballistic codes.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1991
Accession Number
ADA238628

Entities

People

  • Albert W. Horst
  • Carl R. Ruth
  • Frederick W. Robbins

Organizations

  • Ballistic Research Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Ammunition
  • Artillery
  • Ballistics
  • Base Pressure
  • Gages
  • Guns
  • Jet Propulsion
  • Measurement
  • Mechanical Engineering
  • Military Research
  • Munitions
  • Muzzle Velocity
  • Pressure Gages
  • Pressure Gradients
  • Projectiles
  • Propellants
  • Propelling Charges

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Computational Modeling and Simulation
  • ballistics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow
  • Space
  • Space - Hall-Effect Thruster