Final report of ALSEP cask cooling feasibility study

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dc.contributor.author Nordquist, B.
dc.date.accessioned 2015-09-09T22:27:02Z
dc.date.available 2015-09-09T22:27:02Z
dc.date.issued 1968
dc.description.abstract This report summarizes the analysis, design, and test activities conducted at Bendix to evaluate the potential ignition source problem of the Radioisotope Thermoelectric Generator (RTG) fuel cask in the presence of the various vehicle fuel vapors and to establish the requirements for reducing the cask surface temperature in a manner consistent with existing flight hardware and KSC capability.
dc.description.statementofresponsibility prepared by B. Nordquist.
dc.description.tableofcontents Introduction -- Test results -- Theoretical and experimental analysis -- Thermal correlation -- Discussion of pre-test analytical studies
dc.format.extent 87 leaves
dc.format.mimetype application/pdf
dc.identifier.other 31111000665891
dc.identifier.uri https://hdl.handle.net/20.500.11753/128
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/ALSEP%20%23250%20-%20ALSEP%20Cask%20Cooling%20Feasibility%20Study_Final_ATM%20763.pdf
dc.subject.lcc TL789.8.U6A5
dc.subject.lcsh Apollo Lunar Surface Experiments Package
dc.subject.lcsh Radioactive substances--Transportation
dc.title Final report of ALSEP cask cooling feasibility study
dc.title.alternative Final report of Apollo Lunar Surface Experiments Package cask cooling feasibility study
dc.title.alternative ALSEP cask cooling feasibility study
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