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LMS reliability FMECA and SPFS

Show simple item record Hiebert, Robert W. 2015-09-09T22:30:08Z 2015-09-09T22:30:08Z 1972
dc.identifier.other 31111000669653
dc.description.abstract Presented herein are the Failure Mode Effects and Criticality Analysis and the Single Point Failure Summary for the Lunar Mass Spectrometer. The "A" Revision was required to include the Lock Out Switching Circuit(see page 174 for description). The "B" Revision is required due to the design change on the Emission Control from a fixed mode ionization voltage (Assy. #151-700) to a multimode ionization voltage (Assy. #151-550).
dc.description.sponsorship Contract No. NAS 9-5829
dc.description.statementofresponsibility prepared by R. Hiebert.
dc.format.extent 166 leaves
dc.format.mimetype application/pdf
dc.language.iso en
dc.publisher Bendix Aerospace Systems Division
dc.relation.ispartofseries ALSEP technical memorandum
dc.subject.lcc TL789.8.U6A5
dc.subject.lcsh Apollo Lunar Surface Experiments Package
dc.subject.lcsh Mass spectrometers
dc.title LMS reliability FMECA and SPFS
dc.title.alternative Lunar Mass Spectrometer reliability failure mode effects and criticality analysis and single point failure
dc.description.version Revision no. B

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    Apollo Lunar Surface Experiment Package (ALSEP) Documents

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