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Heat loss through LSM flight cable

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dc.contributor.author Psaros, G.
dc.date.accessioned 2015-09-09T22:27:03Z
dc.date.available 2015-09-09T22:27:03Z
dc.date.issued 1968
dc.identifier.other 31111000665990
dc.identifier.uri https://hdl.handle.net/20.500.11753/138
dc.description.abstract The heat loss through the constantan section of the LSM cable has been analyzed by a closed analytical solution. This solution includes the losses due to conduction and radiation. The effect of the radiation losses from the cable both internal and external to the EGFU package are also accounted for. The heat loss during lunar night was computed using boundary conditions consistent with the ALSEP environment, and found to be .25 watts.
dc.description.statementofresponsibility [prepared by G. Psaros].
dc.format.extent 4 leaves
dc.format.mimetype application/pdf
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%23260%20-%20Heat%20Loss_LSM%20Flight%20Code_ATM%20741.pdf
dc.subject.lcc TL789.8.U6A5
dc.subject.lcsh Apollo Lunar Surface Experiments Package
dc.subject.lcsh Lunar Surface Magnetometer
dc.subject.lcsh Electronic apparatus and appliances--Temperature control
dc.title Heat loss through LSM flight cable
dc.title.alternative Heat loss through Lunar Surface Magnetometer flight cable


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    Apollo Lunar Surface Experiment Package (ALSEP) Documents

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