The durability of the SSME turbine is strongly affected by the temperature profile leaving the preburner. A reacting flow computer model to predict the turbine inlet temperature profile was used. Calculations were made by using a reacting flow code, to assess the sensitivity of the turbine inlet temperature profile to variations in the flow entering the SSME preburner.
SSME Fuel Preburner Two-Dimensional Analysis
Structural Integrity and Durability of Reusable Space Propulsion Systems ; 1985 ; Cleveland, Ohio, US
1985-05-01
Conference paper
No indication
English
SSME Fuel Preburner Injector Characterization
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