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Concurrent Design used in the Design of Space InstrumentsAt 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.
Document ID
19990071165
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Oxnevad, Knut I.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Date Acquired
August 19, 2013
Publication Date
July 1, 1998
Publication Information
Publication: Proceedings of the Seventh International Space University Alumni Conference
Subject Category
Spacecraft Instrumentation
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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