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Interface requirements for electric propulsion power processing equipmentPower processor interfaces, internal functions, and design techniques established for the 30-cm ion engine power processor are discussed. The interfaces include the ion engine interface, the spacecraft interface, source/load interactions, protection, and optimization criteria. In the analysis, particular attention is given to the interaction and protection aspects. A breadbord system designed and built for the 30-cm ion engine is discussed which will be used as an engineering tool to establish guidelines for electric propulsion systems.
Document ID
19740029493
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Biess, J. J.
Schoenfeld, A. D.
Goldin, D. S.
(TRW Systems Group Redondo Beach, Calif., United States)
Shank, J. H.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 7, 2013
Publication Date
October 1, 1973
Subject Category
Auxiliary Systems
Report/Patent Number
AIAA PAPER 73-1108
Meeting Information
Meeting: Electric Propulsion Conference
Location: Lake Tahoe, NV
Start Date: October 31, 1973
End Date: November 2, 1973
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
74A12243
Funding Number(s)
CONTRACT_GRANT: NAS3-14383
Distribution Limits
Public
Copyright
Other

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