SOME EFFECTS OF ELECTRON IRRADIATION AND TEMPERATURE ON SOLAR CELL PERFORMANCE,

Abstract

The ANNA 1B geodetic satellite was launched into a 600 nautical mile, 50 degree inclination orbit on October 31, 1962. Portions of VI curves of the flashing light circuit were subsequently determined from telemetry records. These data are presented as the solid line portions of Figure 1 for two days and for 29 days after launch. Examination of these curves indicates the change in both voltage and current which occur after irradiation. The effect of temperature is also indicated. Therefore, a study of solar cell performance after irradiation and as a function of cell temperature was undertaken. A quantitative analysis of these effects is presented, compared with experimental results and the design capabilities of these techniques evaluated.

Document Details

Document Type
Technical Report
Publication Date
May 15, 1963
Accession Number
AD0651013

Entities

People

  • E. L. Ralph
  • J. H. Martin
  • J. W. Teener

Organizations

  • Johns Hopkins University Applied Physics Laboratory

Tags

DTIC Thesaurus Topics

  • Artificial Satellites
  • Cells
  • Cooperation
  • Electron Irradiation
  • Electronics
  • Electrons
  • Geodetic Satellites
  • Nautical
  • Solar Cells
  • Space Systems
  • Spacecraft
  • Telemetry
  • Vehicles

Readers

  • Aerospace Test and Evaluation
  • Pulsed Power and Plasma Physics.
  • Space Exploration and Orbital Mechanics.

Technology Areas

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