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Final report ALSEP Boydbolt fastener design verification program preliminary dynamic tests

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dc.contributor.author Foster, Robert.
dc.date.accessioned 2015-09-09T22:27:13Z
dc.date.available 2015-09-09T22:27:13Z
dc.date.issued 1968
dc.identifier.other 31111000666907
dc.identifier.uri http://hdl.handle.net/20.500.11753/206
dc.description.abstract These preliminary dynamic tests were run subsequent to the Boydbolt static tests. The purpose was to (1) check out the revised installation technique (procedure 2. 33597 5, Revision C), (2.) examine the Boydbolt with the hardened spindles (CA 2.773-14-1) as compared with the regular bolt (CA 2773-14), and (3) further test the effect of Mylar insulation material on bolt preload.
dc.description.statementofresponsibility prepared by R. Foster.
dc.format.extent 13 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/ALSEP%20%23293%20-%20Boydbolt%20Fast%20Design%20Veri%20Test_Final_Addend_ATM%20807.pdf
dc.subject.lcc TL789.8.U6A5
dc.subject.lcsh Apollo Lunar Surface Experiments Package.
dc.subject.lcsh Fasteners.
dc.title Final report ALSEP Boydbolt fastener design verification program preliminary dynamic tests
dc.title.alternative ALSEP Boydbolt fastener design verification program preliminary dynamic tests
dc.title.alternative Final report Apollo Lunar Surface Experiments Package Boydbolt fastener design verification program preliminary dynamic tests


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    Apollo Lunar Surface Experiment Package (ALSEP) Documents

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