NASA NTRS · 19670059983
Ion rocket engine propellant systems and high voltage electrical isolation studies.
Abstract
Cesium propellant systems utilizing surface tension to position and transfer liquid propellant in zero-g environment studied with high voltage electrical isolation methods
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Barcatta, F., Hodges, L., Kosky, A. N., Seele, G. D., Trump, G. E., Wiser, H. L.. 1967-09-01. Ion rocket engine propellant systems and high voltage electrical isolation studies.. https://ntrs.nasa.gov/citations/19670059983
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