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Shuttle Main Propulsion System LH2 Feed Line and Inducer SimulationsThis viewgraph presentation includes simulations of the unsteady flow field in the LH2 feed line, flow line, flow liner, backing cavity and inducer of Shuttle engine #1. It also evaluates aerodynamic forcing functions which may contribute to the formation of the cracks observed on the flow liner slots. The presentation lists the numerical methods used, and profiles a benchmark test case.
Document ID
20030064034
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Daniel Dorney (Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Jeffry Rothermel (Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Date Acquired
August 21, 2013
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: NASA/MSFC Fluids Workshop
Location: Huntsville, AL
Country: US
Start Date: November 19, 2002
End Date: November 21, 2002
Sponsors: Marshall Space Flight Center
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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