A simplified model is presented of the space shuttle main engine (SSME) dynamics valid within the range of operation of the engine. This model is obtained by linking the linearized point models obtained at 25 different operating points of SSME. The simplified model was developed for use with a model-based diagnostic scheme for failure detection and diagnostics studies, as well as control design purposes.
Simplified Dynamic Model of the Space Shuttle Main Engine
1991
12 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Failure analysis , Space shuttle main engine , Combustion chambers , Computerized simulation , Engine control , Mathematical models , Algorithms , Control systems design , Dynamic models , Engine monitoring instruments , Linear systems , Propulsion system configurations , Steady state
A simplified dynamic model of Space Shuttle Main Engine
NTRS | 1991
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