Heat loss through LSM flight cable

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.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.identifier.other	31111000665990
dc.identifier.uri	https://hdl.handle.net/20.500.11753/138
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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