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 |
|