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Optimization of RAE satellite boom deployment timingRadio Astronomy Explorer satellite boom deployment method resulting in gravity gradient capture, emphasizing role of predeployment attitude and antenna Vee angle
Document ID
19700065740
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bowers, E. J., Jr.
Williams, C. E.
Date Acquired
August 5, 2013
Publication Date
September 1, 1970
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 69-920
Report Number: AIAA PAPER 69-920
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS AND AMERICAN ASTRONAUTICAL SOCIETY, ASTRODYNAMICS CONFERENCE
Location: PRINCETON, NJ
Start Date: August 20, 1969
End Date: August 22, 1969
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AMERICAN ASTRONAUTICAL SOCIETY
Accession Number
70A41856
Funding Number(s)
CONTRACT_GRANT: NAS5-9753-20
Distribution Limits
Public
Copyright
Other

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