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Multi-Phase Modeling of Rainbird Water InjectionThis paper describes the use of a Volume of Fluid (VOF) multiphase model to simulate the water injected from a rainbird nozzle used in the sound suppression system during launch. The simulations help determine the projectile motion for different water flow rates employed at the pad, as it is critical to know if water will splash on the first-stage rocket engine during liftoff.
Document ID
20140010060
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Vu, Bruce T.
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Moss, Nicholas
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Sampson, Zoe
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Date Acquired
July 23, 2014
Publication Date
June 16, 2014
Subject Category
Fluid Mechanics And Thermodynamics
Launch Vehicles And Launch Operations
Report/Patent Number
KSC-E-DAA-TN14951
Report Number: KSC-E-DAA-TN14951
Meeting Information
Meeting: AIAA Fluid Dynamics Conference
Location: Atlanta, GA
Country: United States
Start Date: June 16, 2014
End Date: June 20, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 709031.01.02.11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Motion Projectile
Volume of Fluid
Rainbird Flow
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