Dispersion-Strengthened Metal Structural Development. Part II.

Abstract

A research program was conducted to investigate structural utilization of oxidation resistant dispersion-strengthened metals (DSM) is described. The program was initiated to assess their use in structures that will experience repeated service at elevated temperatures in the range of 1400 F to 2400 F. The entire effort is divided into six phases to provide an orderly investigation in the areas of (1) structural design requirements, (2) material survey and evaluation, (3) structural design allowables, (4) structural test assembly design, (5) structural assembly evaluation through tests, and (6) evaluation of material changes caused by the cyclic tests. Results of Phases IV and V are described. The selection, design, fabrication, and testing of a representative DSM structural assembly are described. The vertical fin of a hypersonic high lift-to-drag reentry vehicle was chosen for demonstration of the structural application of DSM. Ni-20Cr-2ThO2 was previously selected in earlier program phases as the most suitable DSM for structural use; this material was employed in a majority of components in the fin test assembly. The completed fin structure had a projected area of 15.7 square feet, and its weight, with test fittings included, was 139 pounds. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 01, 1973
Accession Number
AD0910317

Entities

People

  • D. H. Killpatrick
  • Read Johnson Jr.

Tags

DTIC Thesaurus Topics

  • Assembly
  • Cyclic Tests
  • Demonstrations
  • Dispersions
  • Fabrication
  • High Lift
  • Materials
  • Oxidation
  • Reentry Vehicles
  • Test And Evaluation
  • Vehicles

Readers

  • Aerodynamics/Aeronautics.
  • Business Analytics
  • Reinforced Composite Materials

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow