Failure mode, effects and criticality analysis of ASE EMI modifications

dc.contributor.author	McGinnis, P.
dc.date.accessioned	2015-09-09T22:27:17Z
dc.date.available	2015-09-09T22:27:17Z
dc.date.issued	1969
dc.description.abstract	Criticality rankings were calculated on the basis of probability of failure, system effect and failure mode distribution. The probability criticality product (PCP) was calculated to indicate the order of criticality for each failure mode. Each potential failure having a high ranking has been considered for corrective action within the Limitations of Schedule, Budget and Weight.
dc.description.statementofresponsibility	prepared by P. McGinnis.
dc.format.extent	7 leaves
dc.format.mimetype	application/pdf
dc.identifier.other	31111000667079
dc.identifier.uri	https://hdl.handle.net/20.500.11753/221
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/31111000667079.pdf
dc.subject.lcc	TL789.8.U6A5
dc.subject.lcsh	Apollo Lunar Surface Experiments Package
dc.subject.lcsh	Geophone
dc.subject.lcsh	Grenade launchers
dc.subject.lcsh	Active Seismic Experiment (Instrument)
dc.title	Failure mode, effects and criticality analysis of ASE EMI modifications
dc.title.alternative	Failure mode, effects and criticality analysis of Active Seismic Experiment EMI modifications

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