NASA NTRS · 19680052463
Attitude control of an electrically propelled spacecraft utilizing the primary thrust system.
Abstract
Computer simulated physical characteristics of electrically propelled spacecraft for selecting and designing attitude control system
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Mankovitz, R. J., Reader, P. D.. 1968-01-01. Attitude control of an electrically propelled spacecraft utilizing the primary thrust system.. https://ntrs.nasa.gov/citations/19680052463
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