Observations of Differential Charging with Meteostat,

Abstract

The behavior of the geosynchronous Meteosat spacecraft in the Earth's shadow throws new light on the topic of the influence of secondary electron emission on differential charging, which could assist understanding of these processes in more general situations. Meteosat F1, a geosynchronous meteorological satellite operated by the European Space Agency, suffered from a number of non-damaging operational anomalies that were attributed to electrostatic discharges caused by differential charging. The second flight model F2 was modified in several ways to reduce its susceptibility to arcing. In addition, two new sensors were included in the payload to monitor the plasma environment and to detect the electrical effects of discharges. Since launch in June 1981 the spacecraft has experienced only a few anomalies attributable to arcing and no electrostatic discharges have been detected by the monitor although that could be a matter of sensitivity. So far the only evidence for the spacecraft charging to significant potentials occurs during eclipse and comes from the plasma environment monitor.

Document Details

Document Type
Technical Report
Publication Date
Jan 25, 1983
Accession Number
ADP002112

Entities

People

  • A. D. Johnstone
  • G. L. Wrenn

Organizations

  • University College London

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Air Force
  • Artificial Satellites
  • Buildings And Structures
  • Electrical Properties
  • Electron Emission
  • Electrons
  • Emission
  • Environment
  • Large Space Structures
  • Meteorological Satellites
  • Payload
  • Photoexcitation
  • Polar Orbits
  • Spacecraft
  • Spacecraft Charging
  • Spacecraft Components

Fields of Study

  • Environmental science

Readers

  • Astronomy and Astrophysics.
  • Aviation Safety Risk Assessment.
  • Electrical Engineering

Technology Areas

  • Microelectronics
  • Microelectronics - Microelectromechanical Systems
  • Space