Performance of Three Ablation Materials During Simulation of Long-Duration Afterbody Heating.

Abstract

An experimental investigation was made to determine the resistance to heat penetration and deformations or buckling of three ablation materials during simulated exposure to lifting vehicle afterbody heating conditions. The ablation materials, which were bonded to inconel cones, were subjected to convective heating at cold-wall heating rates ranging from 4 to 40 Btu/sq ft-sec (45 to 454 kW/sq m) in arc jet streams of air and nitrogen. The ablation materials tested were a molded epoxy-based composite and a silicone elastomeric with and without honeycomb reinforcement. For the test conditions of the investigation, models with the epoxy-based composite and the unreinforced silicone elastomeric developed buckles in the ablation material; two models of the epoxy-based composite failed catastrophically. The honeycomb reinforcement in the silicone elastomeric was beneficial in restraining thermal expansion and maintaining char integrity. Except for tests in nitrogen, the silicone elastomerics provided the best resistance to heat penetration.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1967
Accession Number
ADA307038

Entities

People

  • Marvin B. Dow
  • Stephen S. Tompkins

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Ablative Materials
  • Aging (Materials)
  • Composite Materials
  • Heat Shields
  • Heat Transfer
  • High Temperature
  • Jet Streams
  • Lifting Reentry Vehicles
  • Mass Flow
  • Material Degradation Processes
  • Materials
  • Materials Processing
  • Measurement
  • Nose Caps
  • Photographs
  • Resistance
  • Spacecraft

Readers

  • Polymer Science and Engineering.
  • Structural Dynamics.
  • Thermal Physics or Thermal Science.