Evaluation Program for Secondary Spacecraft Cells. Initial Evaluation Tests of Eagle-Picher Industries, Incorporated 3.0 Ampere-Hour Nickel-Cadmium Spacecraft Cells,

Abstract

The purpose of this evaluation test program is to insure that all cells put into the life cycle program are of high quality by the screening of cells found to have electrolyte leakage, internal shorts, low capacity, or inability of any cell to recover its open circuit voltage above 1.150 volts on the cell short test. The five cells were purchased by Philco-Ford for the National Aeronautics and Space Administration, Goddard Space Flight Center. The cells are to be evaluated for a proposed flight battery on the Synchronous Meteorological Satellite to be launched in 1974. These cells are rated at 3.0 ampere-hours (EP Lot no. 4), contain double ceramic seals, and were fitted with pressure transducers prior to testing. Test limits specify those values in which a cell is to be terminated from a particular charge or discharge. Requirements are referred to as normal expectant values based on past performance of aerospace nickel-cadmium cells with demonstrated life characteristics.

Document Details

Document Type
Technical Report
Publication Date
Oct 29, 1973
Accession Number
AD0771347

Entities

People

  • J. D. Harkness

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Aeronautics
  • Artificial Satellites
  • Cycles
  • Earth Observation Satellites
  • Electrolytes
  • Flight
  • Life Cycles
  • Meteorological Satellites
  • Pressure Transducers
  • Satellite Buses
  • Space Flight
  • Spacecraft
  • Spacecraft Components
  • Test And Evaluation
  • Transducers

Readers

  • Battery Technology and Engineering
  • Space Exploration and Orbital Mechanics.

Technology Areas

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