Charging of a Man in the Wake of the Shuttle

Abstract

Charging of the DMSP F6 and F7 satellites is shown to result from the combined effects of high flux of high energy auroral electrons and low ambient background ion density. POLAR computer code calculations are presented which show that a shuttle size object will charge more than 3000 volts negative under these charging conditions. The highly charged shuttle accelerates ions to the shuttle potential producing a high energy mono-energetic plasma environment near the shuttle. During these charging events, an astronaut performing EVA will charge with its ion collection orbit limited. Material secondary properties will produce differential charging on the astronaut of the same magnitude as the shuttle charging potential. NASCAP computer code calculations of EMU charging in the near shuttle environment show differential voltage of 2600 volts and overall charging 1000 volts more negative than the shuttle will occur.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1986
Accession Number
ADA182789

Entities

People

  • G. A. Jongeward
  • I. Katz
  • J. R. Lilley Jr.
  • M. J. Mandell

Tags

Communities of Interest

  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Artificial Satellites
  • Current Density
  • Dielectric Permittivity
  • Electric Fields
  • Electron Emission
  • Electron Flux
  • Electrons
  • Emission
  • Equations
  • Geosynchronous Orbits
  • Meteorological Satellites
  • Protons
  • Spacecraft
  • Spacecraft Charging
  • Spacecraft Orbits
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Plasma Physics / Magnetohydrodynamics
  • Space Exploration and Orbital Mechanics.

Technology Areas

  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster