Telescoping Cavitator

Abstract

This patent application discloses a high speed underwater projectile configuration that includes a cylindrical telescoping cavitator design capable of providing projectile nose shape change where such change to the projectile nose tip geometry results in supercavitation and a concomitant vaporous cavity in the water that reduces projectile drag resistance while maximizing projectile range and where the projectile nose tip further includes a retractable cavitator piston feature. The projectile nose is designed to house a cylindrical cavitator piston that protrudes forward from the projectile and is held in place until launch. Velocity induced hydrodynamic forces on the forward face of this cavitator piston cause the piston to start moving aft and to gradually cause the piston to retract into the projectile nose, until a larger, secondary cavitator is exposed to the vaporous cavity.

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Document Details

Document Type
Technical Report
Publication Date
Mar 13, 2009
Accession Number
ADD020419

Entities

People

  • Thomas J. Gieseke

Organizations

  • United States Department of the Navy

Tags

DTIC Thesaurus Topics

  • Bodies
  • Drag
  • Geometry
  • Inventions
  • Low Drag
  • Nose Tips
  • Noses
  • Patent Applications
  • Patents
  • Projectile Noses
  • Projectiles
  • Resistance
  • Retractable
  • Technology Transfer
  • Undersea Warfare
  • Underwater Projectiles
  • Warfare

Fields of Study

  • Physics

Readers

  • Explosive Engineering.
  • Fluid Mechanics and Fluid Dynamics.
  • Marine Propulsion Engineering and Naval Architecture

Technology Areas

  • Space
  • Space - Hall-Effect Thruster
  • Space - Spacecraft Maneuvers