LSPE Explosive Package stowage and deployment thermal constraints

dc.contributor.author	Toelle, Dan.
dc.date.accessioned	2015-09-09T22:30:15Z
dc.date.available	2015-09-09T22:30:15Z
dc.date.issued	1971
dc.description.abstract	This ATM revision presents a supplement to the study of the LSPE High Explosive Package and transport frame stowage thermal constraints subsequent to LM touchdown and prior to lunar deployment. In addition, lunar deployment thermal constraints are presented for deployment of the individual H. E. packages. This revision is meant to accompany the original ATM-1002.
dc.description.statementofresponsibility	prepared by D. Toelle.
dc.description.version	Revision no. A
dc.description.version	Revision no. A
dc.format.extent	14 leaves
dc.format.mimetype	application/pdf
dc.identifier.other	31111000670131
dc.identifier.uri	https://hdl.handle.net/20.500.11753/396
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/31111000670131.pdf
dc.subject.lcc	TL789.8.U6A5
dc.subject.lcsh	Apollo Lunar Surface Experiments Package
dc.subject.lcsh	Lunar Seismic Profiling Experiment
dc.subject.other	Apollo 17
dc.title	LSPE Explosive Package stowage and deployment thermal constraints
dc.title.alternative	Lunar Seismic Profiling Experiment stowage and deployment thermal constraints

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