Free-Flight Test Results on the Performance of Cork as a Thermal Protection Material.

Abstract

A series of flight tests was initiated by the Langley Research Center for the purpose of testing ablative cork as a lightweight thermal protection material. These flight tests were conducted aboard NASA flight vehicles in the low-heating-rate environment of the afterbody regions. The test conditions covered a range of altitudes to 482,000 feet and velocities to 17,900 feet per second. The test results show that cork can provide adequate thermal protection for a long-time, low-heating-rate environment. p4

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1964
Accession Number
ADA309312

Entities

People

  • Randolph A. Graves Jr.
  • Thomas E. Walton Jr.

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Heating
  • Air Force
  • Boundary Layer
  • Calorimeters
  • Dynamic Pressure
  • Free Flight
  • Heat Transfer
  • Instrumentation
  • Materials
  • Measurement
  • Photographs
  • Reconnaissance Vehicles
  • Recovery Vehicles
  • Solid Propellants
  • Surface Temperature
  • Trajectories
  • Vehicles

Fields of Study

  • Physics

Readers

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