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NASA Ground-based Layered Pressure Vessels Materials ReportA significant portion of Layered Pressure Vessels (LPVs) manufactured for NASA in the 1950s and ’60s are of non-code construction. These vessels were constructed to the standards of individual manufacturers rather than an industry or consensus standard and often contain legacy or proprietary materials, which have poor or no characterization. Obtaining correct material properties is the first step in assuring vessel safety and predicting life and critical failure modes before they happen. This report details the efforts of the LPV Project related to material properties and characterization. The goal in testing materials from deconstructed vessels was to provide material characterization utilizing modern test methods that would give a strong probabilistic base as an option for future analysis. ASTM E1820, Standard Test Method for Measurement of Fracture Toughness was used for fracture toughness; ASTM E1921, Standard Test Method for Determination of Reference Temperature, T0, for Ferritic Steels in the Transition Range for transition temperature; and ASTM E647, Standard Test Method for Measurement of Fatigue Crack Growth Rates for fatigue crack growth. Particular focus was placed on determination of transition temperature through evaluation of the T0 reference temperature in accordance with ASTM E1921. Transition temperature testing allows for a probabilistic analysis of vessel materials that may be operating at temperatures below the transition from ductile tearing to brittle cleavage failure. This test method was not available at the time of construction and has proved invaluable to the characterization of older ferritic steels. The values reported are specific to the largest body of materials found in the current NASA fleet, but do not claim to be all inclusive. As demonstrated in this report, some materials contain extreme lot-to-lot variability. In some cases, this can be comfortably bounded by worst case probabilistic methods, however it is always recommended that vessel specific data be collected in as much depth as possible to ensure correct assumptions and avoid unduly restricting vessel usage.
Document ID
20210019043
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Ronald Levi Shelton
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Date Acquired
July 22, 2021
Publication Date
September 16, 2022
Subject Category
Metals And Metallic Materials
Report/Patent Number
NASA/TM-20210019043
Funding Number(s)
PROJECT: 817091.30.50.62.01
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
Keywords
Layered Pressure Vessel
Fracture Toughness
Ductile-Brittle Transition
E1921
LPV
Steels
Ferritic Steel
E1820
E8
Chemistry
Material Properties
Charpy
Weld
Tensile
Fitness for Service
Pressure Systems
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