BURNUP ENHANCEMENT FOR RE-ENTERING NAP SYSTEMS,

Abstract

The feasibility of enhancing the atmospheric burnup of a ZrH-uranium nuclear fuel upon reentry from orbit by addition of small amounts of alloying elements to the fuel was studied. Thirty-eight different modified fuel compositions were prepared and evaluated. The effects of various additives on fluidity, fabricability, ease of hydriding, hardness, and microstructure of the fuel alloy were determined. Thirty-two separate model fuel elements representing 25 most promising alloys based upon their apparent fluidity and ease of hydriding were exposed to simulated re-entry conditions in the exhaust of an oxygen-hydrogen rocket motor. Samples were exposed for 2.5 to 8.0 seconds at a stagnation heat flux level of approximately 370 Btu/(sq ft) (sec). Ablation was noted in all samples. Under the test conditions imposed, the products of ablation of the reference hydride fuel were definitely molten. A phenomenology of the ablation of the reference hydride fuel was described in some detail. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1963
Accession Number
AD0423411

Entities

People

  • Ellis L. Foster Jr.

Organizations

  • Battelle Memorial Institute

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Ablation
  • Additives (Chemicals)
  • Elements
  • Hardness
  • Heat Flux
  • Hydrogen
  • Microstructure
  • Nuclear Fuels
  • Rocket Engines
  • Rockets

Fields of Study

  • Materials science

Readers

  • Electrochemical Engineering/ Fuel Cell Technologies
  • Petroleum Engineering
  • Thermal Physics or Thermal Science.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster
  • Space - Orbital Debris