ALSEP reliability mathematical model and prediction addendum 1 HFE

Hiebert, Robert W.

dc.contributor.author	Hiebert, Robert W.
dc.date.accessioned	2015-09-09T22:30:26Z
dc.date.available	2015-09-09T22:30:26Z
dc.date.issued	1971
dc.identifier.other	31111000671444
dc.identifier.uri	https://hdl.handle.net/20.500.11753/468
dc.description.abstract	This addendum covers the effect on the prediction of HFE due to changes in the electronic design.
dc.description.statementofresponsibility	prepared by R. W. Hiebert.
dc.format.extent	3 leaves
dc.format.mimetype	application/pdf
dc.language.iso	en
dc.publisher	Bendix Aerospace Systems Division
dc.relation.ispartofseries	ALSEP technical memorandum ; 274
dc.source.uri	https://www.lpi.usra.edu/lunar/ALSEP/pdf/31111000671444.pdf
dc.subject.lcc	TL789.8.U6A5
dc.subject.lcsh	Apollo Lunar Surface Experiments Package
dc.subject.lcsh	Lunar heat flow
dc.subject.lcsh	Heat Flow Experiment
dc.title	ALSEP reliability mathematical model and prediction addendum 1 HFE
dc.title.alternative	Apollo Lunar Surface Experiments Package reliability mathematical model and prediction addendum 1 Heat Flow Experiment
dc.description.version	Revision no. G-1