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Tank System Integrated Model: A Cryogenic Tank Performance Prediction ProgramAccurate predictions of the thermodynamic state of the cryogenic propellants, pressurization rate, and performance of pressure control techniques in cryogenic tanks are required for development of cryogenic fluid long-duration storage technology and planning for future space exploration missions. This Technical Memorandum (TM) presents the analytical tool, Tank System Integrated Model (TankSIM), which can be used for modeling pressure control and predicting the behavior of cryogenic propellant for long-term storage for future space missions. Utilizing TankSIM, the following processes can be modeled: tank self-pressurization, boiloff, ullage venting, mixing, and condensation on the tank wall. This TM also includes comparisons of TankSIM program predictions with the test data andexamples of multiphase mission calculations.
Document ID
20170005533
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Bolshinskiy, L. G.
(Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA) Huntsville, AL, United States)
Hedayat, A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hastings, L. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Sutherlin, S. G.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Schnell, A. R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Moder, J. P.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
June 13, 2017
Publication Date
April 1, 2017
Subject Category
Spacecraft Propulsion And Power
Engineering (General)
Report/Patent Number
M-1431
NASA/TM-2017-218239
Distribution Limits
Public
Copyright
Public Use Permitted.
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