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Concurrent engineering of an infrared telescope system
2011
Optical Modeling and Performance Predictions V
A concurrent engineering approach to the design and analysis of a space-borne Electro-Optical (EO) sensor is presented. A detailed design of an infrared telescope payload is developed by an interdisciplinary team of mechanical, structural, thermal, and optical engineers using a Simulation Driven Engineering (SDE) software environment. The telescope payload design is also integrated with a conceptual level design of the space segment of a mission that incorporates the payload. The flow of the
doi:10.1117/12.894979
fatcat:e74cm4kyyraznhqyzsomciddnm