LMS reliability FMECA and SPFS

Hiebert, Robert W.

dc.contributor.author	Hiebert, Robert W.
dc.date.accessioned	2015-09-09T22:30:08Z
dc.date.available	2015-09-09T22:30:08Z
dc.date.issued	1972
dc.identifier.other	31111000669653
dc.identifier.uri	https://hdl.handle.net/20.500.11753/348
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.source.uri	https://www.lpi.usra.edu/lunar/ALSEP/pdf/31111000669653.pdf
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