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Attitude control of an electrically propelled spacecraft utilizing the primary thrust system.Computer simulated physical characteristics of electrically propelled spacecraft for selecting and designing attitude control system
Document ID
19680052463
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mankovitz, R. J.
Reader, P. D.
Date Acquired
August 4, 2013
Publication Date
January 1, 1968
Publication Information
Publisher: AMERICAN SOCIETY OF MECHANICAL ENGINEERS,
Subject Category
Space Vehicles
Meeting Information
Meeting: ANNUAL AVIATION AND SPACE CONFERENCE
Location: BEVERLY HILLS, CA
Start Date: June 16, 1968
End Date: June 19, 1968
Accession Number
68A33435
Distribution Limits
Public
Copyright
Other

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