Accession Number : ADA302033

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

Descriptive Note : Contract rept.,

Corporate Author : MCDONNELL DOUGLAS CORP ST LOUIS MO

Personal Author(s) : Ellis, D. A. ; Pagel, L. L. ; Schaeffer, D. M.

PDF Url : ADA302033

Report Date : MAR 1978

Pagination or Media Count : 157

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.

Descriptors :   *HEAT SHIELDS, *HYPERSONIC AIRCRAFT, *AIRCRAFT PANELS, *LIQUID COOLING, OPTIMIZATION, ALUMINUM ALLOYS, STRUCTURAL ANALYSIS, FABRICATION, RADIATIVE TRANSFER, CRACK PROPAGATION, SHEAR STRESSES, COOLING AND VENTILATING EQUIPMENT, COOLANTS, DESIGN CRITERIA, HEAT FLUX, AEROTHERMODYNAMICS, SURFACE TEMPERATURE, SKIN(STRUCTURAL), AERODYNAMIC HEATING, THERMAL CYCLING TESTS, DYNAMIC PRESSURE, THERMAL STRESSES, HEAT SINKS, FATIGUE TESTS(MECHANICS), AXIAL LOADS, CYCLIC LOADS, SANDWICH PANELS, HONEYCOMB STRUCTURES, ETHYLENE GLYCOL, THERMAL INSULATION, HEAT RESISTANT ALLOYS, STRUCTURAL INTEGRITY.

Subject Categories : Research and Experimental Aircraft
      Thermodynamics
      Air Condition, Heating, Lighting & Ventilating

Distribution Statement : APPROVED FOR PUBLIC RELEASE