Shock and Vibration Testing of a Rocket-Boosted RF Decoy

Abstract

In order to evaluate the survivability of the RF payload, associated avionics, and structural integrity of the FLYRT RF decoy, a series of vibration and shock tests were performed. Presented are the experiments and their subsequent results

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Document Details

Document Type
Technical Report
Publication Date
May 18, 1994
Accession Number
ADA279923

Entities

People

  • Gregory S. Page
  • Ronald B. Walden

Organizations

  • United States Naval Research Laboratory

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Air Guns
  • Airframes
  • Avionics
  • Booster Rocket Engines
  • Frequency
  • Military Research
  • Resonant Frequency
  • Rockets
  • Shock
  • Shock Response Spectra
  • Shock Tests
  • Simulators
  • Spectra
  • Structural Integrity
  • Vehicles
  • Vibration

Readers

  • Aerospace Test and Evaluation
  • Missile Defense Systems.