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Optimization of RAE satellite boom deployment timing.Radio Astronomy Explorer satellite boom deployment method resulting in gravity gradient capture, emphasizing role of predeployment attitude and antenna Vee angle
Document ID
19690061361
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bowers, E. J., Jr.
Williams, C. E.
Date Acquired
August 5, 2013
Publication Date
August 1, 1969
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 69-920
Report Number: AIAA PAPER 69-920
Meeting Information
Meeting: ASTRODYNAMICS CONFERENCE
Location: PRINCETON, NJ
Start Date: August 20, 1969
End Date: August 22, 1969
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS AND AMERICAN ASTRONAUTICAL SOCIETY
Accession Number
69A39350
Funding Number(s)
CONTRACT_GRANT: NAS9-753-20
Distribution Limits
Public
Copyright
Other

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