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Optimized Heat Interception for Cryogen Tank Support StructureWe consider means for using the cooling available in boil-off gas to intercept heat conducted through the support structure of a cryogen tank. A one-dimensional model of the structure coupled to a gas stream gives an analytical expression for heat leak in terms of flow rate for temperature independent properties and laminar flow. A numerical model has been developed for heat transfer on a thin cylindrical tube with an attached vent line. The model is used to determine the vent path layout that will minimize heat flow into the cryogen tank. The results are useful for a number of applications, but the one of interest in this study is the minimization of the boil-off in large cryopropellant tanks in low Earth and low lunar orbit.
Document ID
20080039140
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Canavan, E. R.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Miller, F. K.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 24, 2013
Publication Date
July 16, 2007
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Cryogenic Engineering Conference
Location: Chatanooga, TN
Country: United States
Start Date: July 16, 2007
End Date: July 20, 2007
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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