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A 30 cm mercury ion thruster moduleLow specific impulse hollow cathode mercury thrustor for deep space electric propulsion, using SERT 2 configuration
Document ID
19710044829
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
King, H. J.
Poeschel, R. L.
Date Acquired
August 6, 2013
Publication Date
April 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 70-1099
Report Number: AIAA PAPER 70-1099
Meeting Information
Meeting: ELECTRIC PROPULSION CONFERENCE
Location: STANFORD, CA
Start Date: August 31, 1970
End Date: September 2, 1970
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
71A25526
Distribution Limits
Public
Copyright
Other

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