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Structural verification of an aged composite reflectorA structural verification program applied to qualifying two heritage composite antenna reflectors for flight on the TOPEX satellite is outlined. The verification requirements and an integrated analyses/test approach employed to meet these requirements are described. Structural analysis results and qualification vibration test data are presented and discussed. It was determined that degradation of the composite and bonding materials caused by long-term exposure to an uncontrolled environment had not severely impaired the integrity of the reflector structures. The reflectors were assessed to be structurally adequate for the intended TOPEX application.
Document ID
19910068945
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lou, Michael C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Tsuha, Walter S.
(JPL Pasadena, CA, United States)
Date Acquired
August 14, 2013
Publication Date
April 1, 1991
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
SAE PAPER 911134
Accession Number
91A53568
Distribution Limits
Public
Copyright
Other

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