ALSEP flight 1 Central Station S-13G thermal coating adhesion investigation

Burns, R.

dc.contributor.author	Burns, R.
dc.date.accessioned	2015-09-09T22:27:12Z
dc.date.available	2015-09-09T22:27:12Z
dc.date.issued	1969
dc.identifier.other	31111000666816
dc.identifier.uri	https://hdl.handle.net/20.500.11753/200
dc.description.abstract	This ATM presents the results of the S-13G thermal coating investigation conducted in support of the ALSEP Flight 1 central station adhesion paint failure. The report includes a summary of the events that occurred during the investigation, a comprehensive review of S-l3G coating application history at BxA, the results of BxA and IITRI coupon tests to determine the cause for the loss of adhesion and establish corrective action, and recommendations for changes to the manufacturing process procedure for subsequent ALSEP painted hardware.
dc.description.statementofresponsibility	prepared by R. Burns.
dc.description.tableofcontents	Summary of Events for Flight 1 S-13G Thermal Coating Adhesion Investigation -- Bendix Test Facilities -- Bendix Test Procedure -- Bendix Test No. 1 -- Bendix Test No. 2 -- Bendix Test No. 3 -- Bendix Test No. 4 -- IITRI Test Program -- Corrective Action for Flight Hardware -- Flight 2 Status -- Flight 3 and Subsequent Flights -- Comments on Application of Test Results -- Additional Proposed S-13G Adhesion Testing
dc.format.extent	56 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%23287%20-%20Flight%201%20CS%20S-13G%20Therm%20Coat%20Adhesion%20Invest_ATM%20831.pdf
dc.subject.lcc	TL789.8.U6A5
dc.subject.lcsh	Apollo Lunar Surface Experiments Package
dc.subject.lcsh	Coatings--Thermal properties
dc.subject.lcsh	Adhesion
dc.title	ALSEP flight 1 Central Station S-13G thermal coating adhesion investigation
dc.title.alternative	Apollo Lunar Surface Experiments Package flight 1 Central Station S-13G thermal coating adhesion investigation