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Electron-bombardment thrusters using liquid- mercury cathodes.Electron bombardment thrustors using liquid mercury cathodes, noting lifetime, propellant and power efficiency, feed system, temperature limits, etc
Document ID
19660045882
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Eckhardt, W. O.
King, H. J.
Knechtli, R. C.
Ward, W.
Date Acquired
August 3, 2013
Publication Date
March 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 66-232
Report Number: AIAA PAPER 66-232
Accession Number
66A25172
Funding Number(s)
CONTRACT_GRANT: NAS3-6262
Distribution Limits
Public
Copyright
Other
Keywords
PROPELLANT TRANSFER
THRUST MEASUREMENT
ELECTRON BOMBARDMENT
LIQUID METAL
ION ENGINE

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