INTEGRAL COVERS FOR SOLAR CELLS,

Abstract

Present integral cover configurations in the 1 to 2 mil thickness range can operate satisfactorily in space for extended time periods. Panel weight reductions of 40 percent are possible for one-year operation in space with a dose equivalent to 10 to the 13th power electrons per square centimeter per day by the use of 4-mil integral covers on thin, drift-field solar cells. A thorough cost-effectiveness analysis of this approach has not been conducted to-date, however. Proper design of these coatings can improve the efficiency of the cells through optimum spectral match and thus eliminates the requirements for adhesives, cover-slip layers, and the associated interference coatings required to reduce ultraviolet-darkening effects on the adhesives. The integral covers exhibit about the same degradation rate as the fused-silica cover slips. These coatings also permit higher temperature operation of solar cells for handling and annealing purposes as well as near-sun mission applications. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 30, 1967
Accession Number
AD0650114

Entities

People

  • J. A. Mcclelland
  • J. F. Wise
  • R. L. Statler

Organizations

  • Air Force Research Laboratory

Tags

DTIC Thesaurus Topics

  • Adhesives
  • Annealing
  • Cells
  • Cooperation
  • Cost Effectiveness
  • Costs
  • Degradation
  • Efficiency
  • Electrons
  • Integrals
  • Military Research
  • Optical Materials
  • Solar Cells
  • Specialists
  • Weight Reduction

Readers

  • Software Engineering
  • Solar Photovoltaics and Thermoelectric Devices.
  • Surface Coatings Technology.

Technology Areas

  • Microelectronics
  • Space