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A study of cryogenic container thermodynamics during propellant transfer. Volume 2 - Final engineering reportThis report describes the results of a study of cryogenic container thermodynamics during propellant transfer. The purpose of this study is to provide analytical and empirical descriptions of the transient phenomena occurring in cryogenic transfer lines and receive tanks during initial propellant transfer. A further basic objective is to identify those conditions which give rise to the possibility of tank implosion, and to establish the procedures and/or systems necessary to eliminate this possibility.
Document ID
19680074446
Acquisition Source
Marshall Space Flight Center
Document Type
Contractor Report (CR)
Authors
R M Vernon
(Lockheed Missiles and Space Company Sunnyvale, California, United States)
J J Brogan
(Lockheed Missiles and Space Company Sunnyvale, California, United States)
Date Acquired
August 4, 2013
Publication Date
October 31, 1967
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Fluid Mechanics and Thermodynamics
Report/Patent Number
NASA-CR-90352
K-14-67-3, V. 2
Report Number: NASA-CR-90352
Report Number: K-14-67-3, V. 2
Accession Number
68X10447
Funding Number(s)
CONTRACT_GRANT: NAS8-20362
Distribution Limits
Public
Copyright
Public Use Permitted.
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