NASA NTRS · 19850019631
SSME Fuel Preburner Two-dimensional Analysis
Abstract
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.
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Thomas J. Vanoverbeke. 1985-05-01. SSME Fuel Preburner Two-dimensional Analysis. https://ntrs.nasa.gov/citations/19850019631
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