Monopole-Quadrupole Model of Spacecraft Charging in Sunlight

Abstract

Geophysics research spacecraft are often covered partially with thin layers of dielectrics such as kapton or thermal blanket materials. Analytical modeling of the charging of a dielectric spacecraft in sunlight needs to go beyond the monopole potential and include a dipole term. If the capacitances of the dielectric 1ayers are sufficiently large and the spacecraft spin rate is sufficiently fast the potentials may be determined on the basis of spin averaged spectra of electron and ion fluxes. In such a condition the potential distribution resembles that of monopole-quadrupole system. We formulate the monopole-quadrupole case and compare it to the monopole-dipole model.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 2005
Accession Number
ADA431710

Entities

People

  • M. Tautz
  • S. T. Lai

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Absorbers (Materials)
  • Advanced Materials
  • Air Force
  • Air Force Research Laboratories
  • Artificial Satellites
  • Astronautics
  • Daylight
  • Electrons
  • Engineered Materials
  • Equations
  • Low Density
  • Military Research
  • Photoelectric Emission
  • Spacecraft
  • Spacecraft Charging
  • Sunlight
  • Vehicles

Fields of Study

  • Physics

Readers

  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Plasma Physics.

Technology Areas

  • Microelectronics
  • Space