The RAE Lightweight Solar Array.

Abstract

The paper traces the development of the RAE lightweight flexible fold-up solar array, culminating in the recent successful tests on a 280W prototype which have qualified the design for 6 years in geostationary orbit. The array embodies a number of unique features, including 125 micrometers silicon solar cells with wraparound contacts, 100 micrometers ceria-stabilized glass coverslips, cementless mounting of cells on the flexible substrate and deployment by a pneumatically actuated telescopic mast. A small version of the array is to be flown on the British X4 satellite in 1974.

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1974
Accession Number
AD0777473

Entities

People

  • F. C. Treble

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Artificial Satellites
  • Cells
  • Congress
  • Deployment
  • Geosynchronous Orbits
  • Lightweight
  • Micrometers
  • Orbits
  • Prototypes
  • Solar Cells
  • Solar Panels
  • Space Systems
  • Spacecraft
  • Substrates
  • Vehicles

Readers

  • Robotics and Automation.
  • Space Exploration and Orbital Mechanics.
  • Surface Engineering/Surface Coating Technology.

Technology Areas

  • Space
  • Space - Satellites
  • Space - Spacecraft Maneuvers