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Functional and physical design of a flight prototype ion engine power conditionerSpace compatible flight prototype ion engine power conditioning system design for Hg thrustor using oxide cathode
Document ID
19700064890
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Benson, G. C.
Garth, D. R.
Muldoon, W. J.
Date Acquired
August 5, 2013
Publication Date
January 1, 1970
Publication Information
Publisher: AMERICAN SOCIETY OF MECHANICAL ENGINEERS,
Subject Category
Propulsion Systems
Meeting Information
Meeting: SPACE SYSTEMS AND THERMAL TECHNOLOGY FOR THE 70''S, AMERICAN SOCIETY OF MECHANICAL ENGINEERS, SPACE TECHNOLOGY AND HEAT TRANSFER CONFERENCE
Location: LOS ANGELES, CA
Start Date: June 21, 1970
End Date: June 24, 1970
Sponsors: SPACE SYSTEMS AND THERMAL TECHNOLOGY FOR THE 70'S
Accession Number
70A41006
Funding Number(s)
CONTRACT_GRANT: JPL-952297
Distribution Limits
Public
Copyright
Other

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