STRUCTURAL TEST OF EXIT-TLM ANTENNA WINDOW, ADVENT, MODEL 8205.

Abstract

The objective of the test is to determine the yield point, the ultimate allowable compressive strength and modulus of elasticity in compression of the fiberglass Exit-TLM AntennaWindow.

Document Details

Document Type
Technical Report
Publication Date
May 09, 1961
Accession Number
AD0801122

Entities

People

  • W. J. Craig

Organizations

  • Lockheed Martin Missiles and Space

Tags

DTIC Thesaurus Topics

  • Antenna Windows
  • Antennas
  • Compression
  • Compressive Strength
  • Elastic Properties
  • Fiberglass
  • Mechanical Properties
  • Modulus Of Elasticity
  • Physical Properties
  • Strength (General)
  • Yield Strength

Readers

  • Database Systems and Applications
  • Electrical Engineering
  • Reinforced Composite Materials