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NASA NTRS · 19710026637

Maximum propellant utilization in an electron-bombardment thruster

Abstract

Maximum propellant utilization in electron bombardment ion thrusters using mercury for propellant

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BibTeXRIS

Kaufman, H. R., Cohen, A. J.. 1971-01-01. Maximum propellant utilization in an electron-bombardment thruster. https://ntrs.nasa.gov/citations/19710026637

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