Structural dynamics analysis report Apollo 14 LRRR

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dc.contributor.author Owens, J. H., Jr.
dc.contributor.author Wadleigh, K. H.
dc.contributor.author Chang, D. C.
dc.date.accessioned 2015-09-09T22:27:30Z
dc.date.available 2015-09-09T22:27:30Z
dc.date.issued 1970
dc.description.abstract The attached structural analysis is divided into three sections. Section I presents the component level stress analysis. This analysis is based on an assumed limit loading of 20g's in any direction. Section II is the dynamics analysis of the structure designed on the basis of the 20g limit load assumption. Section II shows that in general, limit loads are below those assumed in Section I, but that exceptional forces do occur in some locations. Section III is a computer analysis of the redundant grid structure based on the load patterns derived in Section II.
dc.description.statementofresponsibility prepared by J. H. Owens, K. K. Wadleigh, D. C. Chang.
dc.description.tableofcontents Component Stress Analysis -- Vibrations and Dynamic Loads Analysis -- Redundant Grid/Frame Analysis
dc.format.extent 138 leaves
dc.format.mimetype application/pdf
dc.identifier.other 31111000668796
dc.identifier.uri https://hdl.handle.net/20.500.11753/275
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/31111000668796.pdf
dc.subject.lcc TL789.8.U6A5
dc.subject.lcsh Apollo Lunar Surface Experiments Package
dc.subject.lcsh Lunar laser ranging
dc.subject.lcsh Laser Ranging Retroreflector Experiment
dc.title Structural dynamics analysis report Apollo 14 LRRR
dc.title.alternative Structural dynamics analysis report Apollo 14 Laser Ranging Retro Reflector
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