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Defect Characterization in a Thin Walled Composite RP-1 Tank: A Case StudyA full scale thin walled composite tank, designed and fabricated for the storage of pressurized RP- I rocket fuel, was fully inspected with digital infrared thermography (IR) during assembly and prior to proof testing. The tank featured a "pill capsule" design with the equatorial bondline being overwrapped on both the inner and outer surfaces. A composite skirt was bonded to the aft dome of the tank to serve as a structural support when the tank was stood on end in service. Numerous anomalies were detected and mapped prior to proof testing, some along bondlines and some scattered throughout the acreage. After the tank was intentionally burst, coupons were cut from the regions including thermographic anomalies. These coupons were again inspected thermographically to document the growth of any indications due to proof testing. Ultrasonic inspections (UT) were also performed on the coupons for comparison to thermography. Several coupons were dissected and micrographed. Relationships between IR and UT indications and the physical nature of the dissected material are presented.
Document ID
20000040166
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Langsing, Matthew D.
(Alabama Univ. Huntsville, AL United States)
Walker, James L., II
(NASA Marshall Space Flight Center Huntsville, AL United States)
Russell, Samual S.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 2000
Subject Category
Quality Assurance And Reliability
Meeting Information
Meeting: 2000 ASNT Spring Conference
Location: Birmingham, AL
Country: United States
Start Date: March 27, 2000
End Date: March 31, 2000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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