Array E uplink redundancy method justification
Array E uplink redundancy method justification
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Date
1971
Authors
Dallaire, Rodney J.
Thomas, D. J.
Journal Title
Journal ISSN
Volume Title
Publisher
Bendix Aerospace Systems Division
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.