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A mechanism for three axis control of an ion thruster arrayThree axis attitude ion thrust vector control mechanism for solar electric propulsion spacecraft, discussing gimbal and translation actuators, array and cabling
Document ID
19700065668
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ferrera, J. D.
Johnson, K. G.
Masek, T. D.
Perkins, G. S.
Date Acquired
August 5, 2013
Publication Date
August 1, 1970
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Auxiliary Systems
Report/Patent Number
AIAA PAPER 70-1156
Accession Number
70A41784
Distribution Limits
Public
Copyright
Other

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