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RSST math models, block diagrams and predictions

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dc.contributor.author Moskowitz, Lee S.
dc.date.accessioned 2015-09-09T22:27:24Z
dc.date.available 2015-09-09T22:27:24Z
dc.date.issued 1970
dc.identifier.other 31111000668432
dc.identifier.uri https://hdl.handle.net/20.500.11753/240
dc.description.abstract The failure rates are listed on reliability worksheets and were adjusted for temperature and stress ratios, and screening reduction factors. The numerical reliability prediction for the RSST two year lunar phase of operation is 0.989. This was determined as shown in the math model from the summation of failure rates of all components in the system, using the negative exponential distribution. The reliability correction factor for the non-operating standby phase of the mission was calculated to be 0.99999.
dc.description.statementofresponsibility prepared by Lee Moskowitz.
dc.format.extent 9 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/31111000668432.pdf
dc.subject.lcc TL789.8.U6A5
dc.subject.lcsh Electric controllers
dc.subject.lcsh Apollo Lunar Surface Experiments Package
dc.title RSST math models, block diagrams and predictions
dc.title.alternative Resettable Solid State Timer math models, block diagrams and predictions


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    Apollo Lunar Surface Experiment Package (ALSEP) Documents

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