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Array E uplink redundancy method justification

Show simple item record Dallaire, Rodney J. Thomas, D. J. 2015-09-09T22:30:25Z 2015-09-09T22:30:25Z 1971
dc.identifier.other 31111000671352
dc.description.abstract This ATM provides the reliability justification for the redundancy method employed in the Array E (Apollo 17) uplink. The Array E uplink employs standby redundancy without cross-over and automatic switch-over after 61 hours in the event of uplink failure.
dc.description.statementofresponsibility prepared by R. J. Dallaire, D. J. Thomas.
dc.format.extent 13 leaves
dc.format.mimetype application/pdf
dc.language.iso en
dc.publisher Bendix Aerospace Systems Division
dc.relation.ispartofseries ALSEP technical memorandum ; 1015
dc.subject.lcc TL789.8.U6A5
dc.subject.lcsh Apollo Lunar Surface Experiments Package
dc.subject.lcsh Aerospace telemetry
dc.title Array E uplink redundancy method justification

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