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ALSEP Array E engineering model subpackage no. 1 with PSE - design limit vibration test results

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dc.contributor.author Thomas, R.
dc.date.accessioned 2015-09-09T22:30:35Z
dc.date.available 2015-09-09T22:30:35Z
dc.date.issued 1972
dc.identifier.other 31111000672202
dc.identifier.uri https://hdl.handle.net/20.500.11753/534
dc.description.abstract The engineering model of array E subpackage no. 1 with PSE (EEM-SP1/PSE) was subjected to the design limit vibration levels as specified for ALSEP. The primary purpose of the test was to verify the structural integrity of the system and to verify that the component environments are consistent with component specifications.
dc.description.statementofresponsibility prepared by R. Thomas.
dc.format.extent 44 leaves
dc.format.mimetype application/pdf
dc.language.iso en
dc.publisher Bendix Aerospace Systems Division
dc.relation.ispartofseries ALSEP technical memorandum ; 1083.
dc.source.uri https://www.lpi.usra.edu/lunar/ALSEP/pdf/31111000672202.pdf
dc.subject.lcc TL789.8.U6A5
dc.subject.lcsh Apollo Lunar Surface Experiments Package
dc.subject.lcsh Passive Seismic Experiment (Instrument)
dc.title ALSEP Array E engineering model subpackage no. 1 with PSE - design limit vibration test results
dc.title.alternative Apollo Lunar Surface Experiments Package Array E engineering model subpackage no. 1 with Passive Seismic Experiment - design limit vibration test results


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  • ALSEP Documents
    Apollo Lunar Surface Experiment Package (ALSEP) Documents

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