Mission Integration Study for Solid Teflon Pulsed Plasma Millipound Propulsion System.

Abstract

The objective of this program is to identify, validate and assess advantages to the Air Force of using high performance pulsed plasma electric propulsion technology for satellite stationkeeping, attitude control, drag make-up, and solar pressure compensation and to develop pulsed plasma propulsion system/spacecraft integration and design criteria.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1980
Accession Number
ADA090514

Entities

People

  • J. M. Sellen
  • M. H. Gran
  • M. N. Huberman
  • R. Pieper
  • S. Zafran

Tags

Communities of Interest

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

DTIC Thesaurus Topics

  • Accuracy
  • Astronautics
  • Control Systems
  • Detectors
  • Electric Power
  • Electric Propulsion
  • Energy
  • Engineers
  • Heat Pipes
  • Ion Propulsion
  • Measurement
  • Mechatronic Engineering
  • Meteorological Satellites
  • Power Converters
  • Repetition Rate
  • Solar Panels
  • Spacecraft

Fields of Study

  • Physics

Readers

  • Aerospace Propulsion Engineering.
  • Systems Analysis and Design

Technology Areas

  • Space
  • Space - Hall-Effect Thruster
  • Space - Satellites
  • Space - Spacecraft Maneuvers