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

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.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.identifier.other	31111000672202
dc.identifier.uri	https://hdl.handle.net/20.500.11753/534
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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