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COST-EFFICIENT STORAGE OF CRYOGENS
Author(s) -
James E. Fesmire,
J. P. Sass,
Zoltan F. Nagy,
S. J. Sojourner,
D. L. Morris,
S. D. Augustynowicz,
J. G. Weisend,
John Barclay,
Susan Breon,
Jonathan Demko,
Michael DiPirro,
J. Patrick Kelley,
Peter Kittel,
Arkadiy Klebaner,
Al Zeller,
Mark Zagarola,
Steven Van Sciver,
Andrew Rowe,
John Pfotenhauer,
Tom Peterson,
Jennifer Lock
Publication year - 2008
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.177
H-Index - 75
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.2908498
Subject(s) - liquid hydrogen , thermal insulation , propulsion , propellant , cryogenics , energy storage , thermal energy storage , materials science , aerospace engineering , mechanical engineering , nuclear engineering , environmental science , process engineering , engineering , hydrogen , composite material , physics , power (physics) , layer (electronics) , quantum mechanics , thermodynamics
NASA's cryogenic infrastructure, which supports launch vehicle operations and propulsion testing, is reaching an age when major refurbishment is required. Key elements of this infrastructure are the large double-walled cryogenic storage tanks used for both space vehicle launch operations and rocket propulsion testing at various NASA field centers. Perlite powder has historically been the insulation material of choice for these applications, but new bulk-fill insulation materials, including glass bubbles and aerogel beads, have been shown to provide improved thermal and mechanical performance. Research was conducted on thermal performance to identify operational considerations and risks associated with using these new materials in large cryogenic storage tanks. The program was divided into three main areas: material testing (thermal conductivity and physical characterization), tank demonstration testing (liquid nitrogen and liquid hydrogen), and system studies (thermal modeling, granular physics, and insul...

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