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Array E uplink redundancy method justification

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dc.contributor.author Dallaire, Rodney J.
dc.contributor.author Thomas, D. J.
dc.date.accessioned 2015-09-09T22:30:25Z
dc.date.available 2015-09-09T22:30:25Z
dc.date.issued 1971
dc.identifier.other 31111000671352
dc.identifier.uri https://hdl.handle.net/20.500.11753/459
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.source.uri https://www.lpi.usra.edu/lunar/ALSEP/pdf/31111000671352.pdf
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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    Apollo Lunar Surface Experiment Package (ALSEP) Documents

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