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NASA NTRS · 19680038893

Thrust efficiencies of electromagnetic engines.

Abstract

Ionized plasma electromagnetic accelerators, noting thrust efficiency variation due to difference between supplied and expelled mass flow rate

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BibTeXRIS

Cann, G. L., Harder, R. L.. 1968-03-01. Thrust efficiencies of electromagnetic engines.. https://ntrs.nasa.gov/citations/19680038893

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