Feasibility Study of a Minimum Caliber Target-Marking Round.

Abstract

The feasibility of a target-marking round capable of being delivered from light aircraft by a forward firing weapon was established. The study produced a marking round design which is 60mm in diameter and uses a sustainer rocket to augment the launch velocity and achieve a constant velocity to target. The round is designed to be fired from a low pressure, semi-recoilless launcher, is fin stabilized, and contains the rocket motor in a tandem configuration behind the marker assembly. Upon approaching the target, a proximity fuze in a nose of the marking round triggers a retrofire charge which expels the marker candle assembly rearward to overcome its forward velocity. This method for retarding the marker assembly was demonstrated successfully by a series of experimental retrofirings, including tests with actual marker candles. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1971
Accession Number
AD0889202

Entities

People

  • Philip A. Saigh
  • Robert H. Jacobson

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Assembly
  • Diameters
  • Feasibility Studies
  • Launchers
  • Physical Properties
  • Proximity Fuzes
  • Rocket Engines
  • Rockets
  • Weapons

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.
  • ballistics.