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Satellite/spacecraft propulsionPropulsion system performance has high leverage for many future missions because of large propellant mass requirements. Relatively small performance improvements can translate into large increases in payload and science return. Contamination control becomes more important as science instruments become more sensitive. This places more emphasis on exhaust plume contamination control. The need for reliable operation and long life places increased importance on health monitoring and control of spacecraft propulsion systems. The need for accurate spacecraft pointing and control increases the need for small impulse-bit thrusters. This presentation is represented by viewgraphs.
Document ID
19910018889
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dowdy, Mack W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Publication Information
Publication: NASA, Washington, Space Transportation Propulsion Technology Symposium. Volume 2: Symposium Proceedings
Subject Category
Spacecraft Propulsion And Power
Accession Number
91N28203
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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