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Positive isolation disconnectA positive isolation disconnect was developed for component replacement in serviced liquid and gaseous spacecraft systems. Initially a survey of feasible concepts was made to determine the optimum method for fluid isolation, sealing techniques, coupling concepts, and foolproofing techniques. The top concepts were then further evaluated, including the fabrication of a semifunctional model. After all tradeoff analyses were made, a final configuration was designed and fabricated for development testing. This resulted in a 6.35 mm (1/4 inch) line and 12.7 mm (1/2 inch) line positive isolation disconnect, each unit consisting of two coupled disconnect halves, each capable of fluid isolation with essentially zero clearance between them for zero leakage upon disconnect half disengagement. An interlocking foolproofing technique was incorporated that prevents uncoupling of disconnect halves prior to fluid isolation.
Document ID
19760007099
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rosener, A. A.
(Martin Marietta Corp. Denver, CO, United States)
Jonkoniec, T. G.
(Martin Marietta Corp. Denver, CO, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-144634
MCR-75-365
Report Number: NASA-CR-144634
Report Number: MCR-75-365
Accession Number
76N14187
Funding Number(s)
CONTRACT_GRANT: NAS9-14376
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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