Space Power Experiments Aboard Rockets SPEAR-3.

Abstract

The SPEAR-3 program was a sounding rocket payload designed to study the interaction of a charged body with the Earth's upper atmosphere with particular reference to the discharging ability of selected active devices carried on the payload. Since some of the devices and natural outgassing provide a source of gaseous effluent release, instrumentation was included to study effluent dispersion around the payload. it was found that neutral gas release was most effective at discharging the payload when it was more negative than 500 V. Electron emission was effective only when the currents driving the body negative were lower than the limited current available from the low perveance devices used. The hollow cathode was an ineffective grounding system on this flight due to cathode poisoning believed to have occurred during the vehicle ascent. The grounding data and HV interactions were diagnosed by a variety of instruments measuring both steady state and transient currents and voltages.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1997
Accession Number
ADA327734

Entities

People

  • W. J. Raitt

Organizations

  • Utah State University

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Artificial Satellites
  • Attitude Control Systems
  • Charged Particles
  • Control Systems
  • Detectors
  • Earth Orbits
  • Electron Density
  • Electron Emission
  • Electrons
  • Emission
  • Field Emission
  • Low Earth Orbits
  • Measurement
  • Photoexcitation
  • Solar Cells
  • Surface Finishing
  • Voltage

Readers

  • Electrical Engineering
  • Missile Defense Systems.
  • Pulsed Power and Plasma Physics.

Technology Areas

  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster
  • Space - Satellites