Array E uplink redundancy method justification

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31111000671352.pdf (495.64 KB)
Date
1971
Authors
Dallaire, Rodney J.
Thomas, D. J.
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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.
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https://hdl.handle.net/20.500.11753/459
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