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Ion rocket engine propellant systems and high voltage electrical isolation studies.Cesium propellant systems utilizing surface tension to position and transfer liquid propellant in zero-g environment studied with high voltage electrical isolation methods
Document ID
19670059983
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Barcatta, F.
Hodges, L.
Kosky, A. N.
Seele, G. D.
Trump, G. E.
Wiser, H. L.
Date Acquired
August 3, 2013
Publication Date
September 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 67-681
Report Number: AIAA PAPER 67-681
Accession Number
67A38712
Funding Number(s)
CONTRACT_GRANT: NAS3-7112
CONTRACT_GRANT: NAS3-2516
CONTRACT_GRANT: NAS7-502
CONTRACT_GRANT: AF 33/615/-1530
Distribution Limits
Public
Copyright
Other
Keywords
PROPELLANT TRANSFER
ION ENGINE
SURFACE TENSION
LIQUID PROPELLANT ROCKET ENGINE
ELECTRIC INSULATION

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