NASA NTRS · 19700065668
A mechanism for three axis control of an ion thruster array
Abstract
Three axis attitude ion thrust vector control mechanism for solar electric propulsion spacecraft, discussing gimbal and translation actuators, array and cabling
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Ferrera, J. D., Johnson, K. G., Masek, T. D., Perkins, G. S.. 1970-08-01. A mechanism for three axis control of an ion thruster array. https://ntrs.nasa.gov/citations/19700065668
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