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LEAM dynamic analysis, Flight Model

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dc.contributor.author Wadleigh, K. H.
dc.date.accessioned 2015-09-09T22:30:20Z
dc.date.available 2015-09-09T22:30:20Z
dc.date.issued 1971
dc.identifier.other 31111000670529
dc.identifier.uri http://hdl.handle.net/20.500.11753/430
dc.description.abstract This ATM gives the results of the dynamic analysis on the LEAM Flight Model Experiment Package. The DVT model dynamic analysis and testing results were presented in ATM 1022, Reference 1. A comparison of the flight model hardware and DVT model hardware is made.
dc.description.statementofresponsibility prepared by K. Wadleigh.
dc.format.extent ii, 53 leaves
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.publisher Bendix Aerospace Systems Division
dc.relation.ispartofseries ALSEP technical memorandum
dc.source.uri http://www.lpi.usra.edu/lunar/ALSEP/pdf/31111000670529.pdf
dc.subject.lcc TL789.8.U6A5
dc.subject.lcsh Apollo Lunar Surface Experiments Package.
dc.subject.lcsh Lunar Ejecta and Meteorites Experiment
dc.title LEAM dynamic analysis, Flight Model
dc.title.alternative Lunar Ejecta and Meteorites Experiment dynamic analysis, Flight Model


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    Apollo Lunar Surface Experiment Package (ALSEP) Documents

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