Radiofrequency Transmission Characteristics of Candidate Ablation Materials for Planetary-Entry-Vehicle Heat Shields.

Abstract

An experimental investigation was conducted to determine the radiofrequency properties of several candidate ablation materials for planetary entry vehicle heat shields. The radiofrequency transmissibility of each ablative material was determined by the real time measurement of the attenuation of a 35 GHz signal while each sample was exposed to a simulated planetary entry environment. The simulated planetary environment was produced by providing a heating rate, pressure, and free stream Mach number in an arc heated supersonic wind tunnel. Recordings of the transmission loss obtained through eacb material during the arc tunnel test and photographs of all test specimens before and after thermal exposure are presented. In addition to the transmission loss measurements, the dielectric properties of most virgin materials were measured at room temperature and are also presented.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1968
Accession Number
ADA306847

Entities

People

  • Andrew J. Chapman
  • Douglas M. Hatcher
  • Melvin C. Gilreath

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Advanced Electronics

DTIC Thesaurus Topics

  • Ablative Materials
  • Acoustic Absorption
  • Anechoic Chambers
  • Dielectric Permittivity
  • Dielectric Properties
  • Free Stream
  • Frequency
  • Heat Shields
  • Heat Transfer
  • Mach Number
  • Materials
  • Measurement
  • Pressure Distribution
  • Radio Frequency
  • Supersonic Wind Tunnels
  • Transmission Loss
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Acoustics.
  • Fluid Dynamics.
  • Thermal Physics or Thermal Science.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow