Failure mode, effects and criticality analysis - Array D Redundant Command Receiver

Fox, T. W.

dc.contributor.author	Fox, T. W.
dc.date.accessioned	2015-09-09T22:30:14Z
dc.date.available	2015-09-09T22:30:14Z
dc.date.issued	1971
dc.identifier.other	31111000670040
dc.identifier.uri	https://hdl.handle.net/20.500.11753/387
dc.description.abstract	The failure mode, effects, and criticality analysis shows, in a systematic way, the effect of part, pin, and receiver redundancy on system performance. Specifically these analyses have identified the only single point failure mechanism, have showed which piece part failure modes result in minor degradation at most and may be eliminated from the reliability calculation, and have verified that Receivers A and B are failure isolated.
dc.description.sponsorship	NASA Contract Number: NAS 9-5829 Subcontract. Number: SC-721
dc.description.statementofresponsibility	summarized by T. W. Fox.
dc.format.extent	81 leaves
dc.format.mimetype	application/pdf
dc.language.iso	en
dc.publisher	Bendix Aerospace Systems Division
dc.relation.ispartofseries	ALSEP technical memorandum
dc.source.uri	https://www.lpi.usra.edu/lunar/ALSEP/pdf/31111000670040.pdf
dc.subject.lcc	TL789.8.U6A5
dc.subject.lcsh	Apollo Lunar Surface Experiments Package
dc.title	Failure mode, effects and criticality analysis - Array D Redundant Command Receiver