Further Study of Techniques for Reducing the Vibration of Rocket Launchers Mounted on Helicopters.

Abstract

The report is concerned with the problem of reducing the steady state vibrations of rocket launchers mounted on helicopters. The report presents a study of the problem with emphasis on developing a small scale demonstration test model, and extending the active vibration absorber theory. (Author Modified Abstract)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1973
Accession Number
AD0758141

Entities

People

  • C. D. Johnson

Organizations

  • United States Army Aviation and Missile Command

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Demonstrations
  • Helicopters
  • Launchers
  • Rocket Launchers
  • Steady State
  • Vibration

Readers

  • Marksmanship and Weaponry.
  • Structural Dynamics.
  • Systems Analysis and Design