A mathematical model of the Space Shuttle Main Engine (SSME) as a complete assembly, with detailed emphasis on LOX and High Fuel Turbopumps is developed. The advantages of both complete engine dynamics, and high fidelity modeling are incorporated. Development of this model, some results, and projected applications are discussed.
SSME structural dynamic model development
1983-12-01
Report
No indication
English
Dynamic Online SSME Schematics
NTIS | 2007
|Dynamic Online SSME Schematics
NTRS | 2007
|SSME environment database development
NTRS | 1987
|AIAA | 1989
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