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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
19670048093
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Eckhardt, W. O.
King, H. J.
Knechtli, R. C.
Ward, J. W.
Date Acquired
August 3, 2013
Publication Date
May 1, 1967
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Propulsion Systems
Accession Number
67A26822
Funding Number(s)
CONTRACT_GRANT: NAS3-6262
Distribution Limits
Public
Copyright
Other
Keywords
THRUST MEASUREMENT
ION ENGINE
PROPELLANT TRANSFER
LIQUID METAL
ELECTRON BOMBARDMENT

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