Heat Pipes for Sodium-Sulfur Batteries

Abstract

The objective of this program was to develop a variable conductance heat pipe (VCHP) for the thermal management of sodium-sulfur batteries. The VCHP maintains the sodium sulfur battery within a specified temperature rise limit (20 C) while the battery discharges a thermal load from 0 watts to 500 watts. A preliminary full scale thermal management design was developed for the sodium- sulfur battery, incorporating the VCHPs and supporting integration hardware. The feasibility of the VCHPs for this application was proved by test. The VCHP developed in Phase I utilized titanium as the heat pipe envelope material, and cesium as the heat pipe working fluid. The wick structure was axial grooves. Analysis and test indicate that the VCHP can provide the passive thermal control necessary for the sodium-sulfur battery. Test data show that with the heat input from Q = 0 watts to Q = 500 watts, the VCHP evaporator temperature increased from 350 C to 385 C. The temperature control range was higher than predicted due to working fluid vapor diffusion into the noncondensible gas and thermal axial conduction into the VCHP reservoir. Analysis has shown that by utilizing VCHPs for passive temperature control, the sodium-sulfur battery cells will have a lower axial delta-T during discharge than a current louver design. The VCHP thermal management package has the potential to be used in geosynchronous earth orbits (GEO) and low earth orbits (LEO).

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1989
Accession Number
ADA212523

Entities

People

  • John R. Hartenstine

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Classification
  • Coefficients
  • Computer Programs
  • Computers
  • Conduction (Heat Transfer)
  • Contracts
  • Deep Space
  • Design Criteria
  • Diffusion Coefficient
  • Earth Orbits
  • Fabrication
  • Heat Pipes
  • Heat Transfer
  • Low Earth Orbits
  • Temperature Control
  • Thermal Conductivity
  • Vapor Pressure

Readers

  • Combustion and Flow Dynamics.
  • Electrochemical Engineering/ Fuel Cell Technologies
  • Thermal Physics or Thermal Science.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster
  • Space - Satellites