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Concurrent Design used in the Design of Space Instruments

Authors :
Oxnevad, Knut I
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

Subjects :
Spacecraft Instrumentation

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