NASA NTRS · 19700064890
Functional and physical design of a flight prototype ion engine power conditioner
Abstract
Space compatible flight prototype ion engine power conditioning system design for Hg thrustor using oxide cathode
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Benson, G. C., Garth, D. R., Muldoon, W. J.. 1970-01-01. Functional and physical design of a flight prototype ion engine power conditioner. https://ntrs.nasa.gov/citations/19700064890
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