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Pressure-volume properties of metallic bellowsMetallic bellows are commonly used as segments of propellant feedlines for rocket-propelled vehicles to accommodate temperature-induced length variations, manufacturing tolerances, and gimbaling of the engines. These bellows sections deform radially and change volume when internal pressure varies, and the magnitude of such deformation is much higher than that for the straight, cylindrical segments of the line. The greater flexibility, or lesser stiffness, of the bellows, decreases the frequency of acoustic oscillations in the line. These acoustic oscillations are a major factor in the so-called POGO phenomena which have plagued most of the larger liquid rocket-propelled vehicles for many years. A method is developed to calculate the change in volume of a bellows due to a change in internal pressure. Results of an experiment are also presented along with a test-analysis comparison. The computer code is included.
Document ID
19890015051
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kiefling, Larry
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1989
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:100365
NASA-TM-100365
Report Number: NAS 1.15:100365
Report Number: NASA-TM-100365
Accession Number
89N24422
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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