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Microelectronics Instrument Products Shock and Vibration Electro-OpticsThe strength analysis report for FRR shall include only revisions to update the strength analysis reports for the flight design configuration. Since there have been no revisions to the design configuration since the PDR and the CDR this report shall consist of re-submitting the analysis previously performed. In addition the motors have been subjected to Sine vibration, Random vibration, and shock per the SXI specification. Both motor/encoders have passed all three tests. There was no evidence of damage to the motor/encoder and the motor/encoder performed as required by the Acceptance test procedure. No degradation was seen between the before and after performance tests. The testing verified the analysis that there were adequate mf@ty margins with regard to structural integrity. Separate reports are available from the test facility and are apart of the FRR submittal.
Document ID
19990026254
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Standard/Specification
Date Acquired
September 6, 2013
Publication Date
March 16, 1994
Subject Category
Electronics And Electrical Engineering
Funding Number(s)
CONTRACT_GRANT: NAS8-39409
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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