Development of Encapsulated Lithium Hydride Thermal Energy Storage for Space Power Systems,

Abstract

Inclusion of thermal energy storage in a pulsed space power supply will reduce the mass of the heat rejection system. In this mode, waste heat generated during the brief high-power burst operation is placed in the thermal store; later, the heat in the store is dissipated to space via the radiator over the much longer nonoperational period of the orbit. Thus, the radiator required is of significantly smaller capacity. Scoping analysis indicates that use of lithium hydride as the thermal storage medium results in system mass reduction benefits for burst periods as long as 800 s. A candidate design for the thermal energy storage component utilizes lithium hydride encapsulated in either 304L stainless steel or molybdenum in a packed-bed configuration with a lithium or sodium-potassium (NaK) heat transport fluid.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1987
Accession Number
ADA190689

Entities

People

  • D. G. Morris
  • J. P. Foote
  • M. Olszewski

Organizations

  • Oak Ridge National Laboratory

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Ceramic Materials
  • Chemistry
  • Energy
  • Energy Storage
  • Heat Energy
  • Heat Of Fusion
  • Heat Transfer
  • Latent Heat
  • Lithium
  • Materials
  • Mechanical Properties
  • Mechanical Working
  • Mechanics
  • Tensile Strength
  • Thermal Conductivity
  • Thermodynamics

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Electrical Engineering
  • Thermal Physics or Thermal Science.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster