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Concurrent Design used in the Design of Space Instruments
- Source :
- Proceedings of the Seventh International Space University Alumni Conference.
- Publication Year :
- 1998
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1998.
-
Abstract
- At the Project Design Center at the Jet Propulsion Laboratory, a concurrent design environment is under development for supporting development and analyses of space instruments in the early, conceptual design phases. This environment is being utilized by a Team I, a multidisciplinary group of experts. Team I is providing study and proposal support. To provide the required support, the Team I concurrent design environment features effectively interconnected high-end optics, CAD, and thermal design and analysis tools. Innovative approaches for linking tools, and for transferring files between applications have been implemented. These approaches together with effective sharing of geometry between the optics, CAD, and thermal tools are already showing significant timesavings.
- Subjects :
- Spacecraft Instrumentation
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Journal :
- Proceedings of the Seventh International Space University Alumni Conference
- Publication Type :
- Report
- Accession number :
- edsnas.19990071165
- Document Type :
- Report