Fluid Flow Analysis of the Ssme High Pressure Fuel and Oxidizer Turbine Coolant Systems by National Aeronautics and Space Adm Nasa

Fluid Flow Analysis of the Ssme High Pressure Fuel and Oxidizer Turbine Coolant Systems

National Aeronautics and Space Adm Nasa

68 pages missing pub info (view editions)

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The objective is to provide improved analysis capability for the Space Shuttle Main Engine (SSME) high pressure fuel and oxidizer turbine coolant systems. Each of the systems was analyzed to determine fluid flow rate and thermodynamic and transpor...

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