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No Vent Tank Fill and Transfer Line Chilldown Analysis by Generalized Fluid System Simulation Program (GFSSP)The purpose of the paper is to present the analytical capability developed to model no vent chill and fill of cryogenic tank to support CPST (Cryogenic Propellant Storage and Transfer) program. Generalized Fluid System Simulation Program (GFSSP) was adapted to simulate charge‐holdvent method of Tank Chilldown. GFSSP models were developed to simulate chilldown of LH2 tank in K‐site Test Facility and numerical predictions were compared with test data. The report also describes the modeling technique of simulating the chilldown of a cryogenic transfer line and GFSSP models were developed to simulate the chilldown of a long transfer line and compared with test data.
Document ID
20140002987
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Majumdar, Alok
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
April 15, 2014
Publication Date
July 29, 2013
Subject Category
Propellants And Fuels
Report/Patent Number
M13-2805
Report Number: M13-2805
Meeting Information
Meeting: Thermal and Fluids Analysis Workshop (TFAWS) 2013
Location: Daytona Beach, FL
Country: United States
Start Date: July 29, 2013
End Date: August 2, 2013
Sponsors: NASA Langley Research Center
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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