Design and Fabrication of a Radiative Actively Cooled Honeycomb Sandwich Structural Panel for a Hypersonic Aircraft.

Abstract

This report presents the results of a study to design and fabricate a radiative actively cooled panel. The panel assembly consists of an external thermal protection system (metallic heat shields and insulation blankets) and an aluminum honeycomb structure.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1978
Accession Number
ADA302033

Entities

People

  • D. A. Ellis
  • D. M. Schaeffer
  • L. L. Pagel

Organizations

  • McDonnell Douglas

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Chemistry
  • Fluid Flow
  • Fuselages
  • Heat Exchangers
  • Heat Transfer
  • Hypersonic Aircraft
  • Manufacturing
  • Materials Science
  • Mechanical Working
  • Mechanics
  • Modulus Of Elasticity
  • Temperature Gradients
  • Test And Evaluation
  • Three Dimensional
  • Transport Aircraft

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Structural Dynamics.

Technology Areas

  • Hypersonics
  • Microelectronics
  • Microelectronics - Graphene
  • Microelectronics - Microelectromechanical Systems