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Filament Wound Metal Lined Propellant Tanks For Future Earth To Orbit Transports
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722234881 Total Pages :34 pages Book Rating :4.2/5 (348 download)
Book Synopsis Filament Wound Metal Lined Propellant Tanks for Future Earth-To-Orbit Transports by : National Aeronautics and Space Administration (NASA)
Download or read book Filament Wound Metal Lined Propellant Tanks for Future Earth-To-Orbit Transports written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-03 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: For future Earth-to-orbit transport vehicles, reusability and lighter weights are sought for the main propellant tanks. To achieve this, a filament wound tank with a metal liner and an intermediate layer of foam-filled honeycomb is proposed. A hydrogen tank is used as an example. To accommodate mismatches in the expansion of liner and overwrap a design is proposed wherin the liner is configured so that the extension of the liner under pressure matches the expected contraction of the same liner due to the presence of a cryogen. In operation, the liner is pressurized at a rate such that the pressure strain matches the contraction due to decrease in temperature. As an alternate approach, compressive pre-stress is placed in the liner such that it will not separate from the overwrap. A finite element program is used to show stresses in the liner and overwrap for various tank pressures for the pre-stressed liner concept. A fracture mechanics analysis is made of the liners to determine tank life. The tank concept shown has a similar weight to the Shuttle external hydrogen tank, but the filament wound tank is expected to be reusable. Integration of the propellant tanks into a future transport vehicle is discussed. Macconochie, Ian O. and Davis, Robert B. and Freeman, William T., Jr. Langley Research Center RTOP 506-49-11-01...
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