Directed Energy Effects on the Flight Path of a Spinning Ballistic Projectile.

Abstract

This thesis will examine the equations of motion for a spinning ballistic projectile. The goal of such an examination is to determine the possible mechanisms by which a directed energy weapon may induce sufficient instability as to significantly alter the projectile's flight path. A ballistic projectile is generally launched with a "fire and forget" philosophy. The desired impact point is determined before firing. It may be possible to alter the projectile in such a way that it fails to follow the desired trajectory thereby missing the intended target. Several variables appear to be worthy of investigation to assess their contribution to a required instability or range reduction. Skin friction drag may be increased from surface roughness generated by a pulsed energy source. The results that this thesis will examine include: impulse generated by the laser interaction, additional Magnus effects and aerodynamic drag. Moment induced instability may also result from these in the form of a Magnus moment or drag torque. Increasing the drag force appears to be the most promising theoretical solution to defeating an incoming spinning ballistic projectile.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1995
Accession Number
ADA303096

Entities

People

  • George S. Capen

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Drag
  • Directed Energy Weapons
  • Drag
  • Equations Of Motion
  • Flight Paths
  • Friction
  • Impact Point
  • Instability
  • Magnus Effect
  • Projectiles
  • Skin Friction
  • Surface Roughness
  • Trajectories
  • Weapons

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Systems Analysis and Design
  • ballistics.

Technology Areas

  • Directed Energy
  • Space
  • Space - Hall-Effect Thruster
  • Space - Orbital Debris
  • Space - Spacecraft Maneuvers