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A 30-cm-diameter, low specific impulse, hollow cathode mercury thrusterLow specific impulse hollow cathode mercury thrustor for deep space electric propulsion, using SERT 2 configuration
Document ID
19700064777
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
King, H. J.
Poeschel, R. L.
Date Acquired
August 5, 2013
Publication Date
August 1, 1970
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 70-1099
Report Number: AIAA PAPER 70-1099
Accession Number
70A40893
Distribution Limits
Public
Copyright
Other

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