NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Fracture control method for composite tanks with load sharing linersThe experimental program was based on the premise that the plastic sizing cycle, which each pressure vessel is subjected to prior to operation, acts as an effective proof test of the liner, screening out all flaws or cracks larger than a critical size. In doing so, flaw growth potential is available for cyclic operation at pressures less than the sizing pressure. Static fracture and cyclic life tests, involving laboratory type specimens and filament overwrapped tanks, were conducted on three liner materials: (1) 2219-T62 aluminum, (2) Inconel X750 STA, and (3) cryoformed 301 stainless steel. Variables included material condition, thickness, flaw size, flaw shape, temperature, sizing stress level, operating stress level and minimum-to-maximum operating stress ratio. From the empirical data base obtained, a procedure was established by which the service life of composite tanks with load sharing liners could be guaranteed with a high degree of confidence.
Document ID
19750021376
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bixler, W. D.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Quality Assurance And Reliability
Report/Patent Number
D180-18850-1
NASA-CR-134758
Report Number: D180-18850-1
Report Number: NASA-CR-134758
Accession Number
75N29449
Funding Number(s)
CONTRACT_GRANT: NAS3-14380
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available