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Low-Profile DiffuserThe propellant tanks used in liquid rockets require pressurization gases in order to maintain tank pressure while the tanks are being drained during engine operation. The pressurization gas, which is typically much warmer than the relatively cold propellants in the tank, must be introduced into the empty ullage space at the top of the tank. The purpose of the diffuser is to control the flow of the gas into the tank in order to prevent direct impingement of the gas on the liquid surface and/or the tank walls. If the diffuser did not perform those tasks, the warm gas can create excess heat transfer causing an increase in the amount of pressurization mass required. Typical diffusers are long vertical cylinders that create a large exit area in order to minimize gas velocities. However, long vertical cylinders limit the amount of liquid that can be loaded into the tank in order not to have the liquid surface near the diffuser. A design goal for a pressurization diffuser is to create uniform flow in order to prevent jets that can impact the liquid surface and/or tank walls. The purpose of the task was to create a diffuser design that had a lower vertical profile (in order to be able to raise the liquid surface) while still maintaining uniform flow.
Document ID
20160008011
Acquisition Source
Marshall Space Flight Center
Document Type
Other
Authors
Martin, Michael A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Nettles, Mindy
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
June 29, 2016
Publication Date
January 1, 2015
Publication Information
Publication: George C. Marshall Space Flight Center Research and Technology Report 2014
Subject Category
Fluid Mechanics And Thermodynamics
General
Launch Vehicles And Launch Operations
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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