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Integrated Design System (IDS) Tools for the Spacecraft Aeroassist/Entry Vehicle Design ProcessThe definition of the Integrated Design System technology focus area as presented in the NASA Information Technology center of excellence strategic plan is described. The need for IDS tools in the aeroassist/entry vehicle design process is illustrated. Initial and future plans for spacecraft IDS tool development are discussed.
Document ID
20020039970
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Olynick, David (NASA Ames Research Center Moffett Field, CA United States)
Braun, Robert (NASA Langley Research Center Hampton, VA United States)
Langhoff, Steven R.
Date Acquired
August 20, 2013
Publication Date
January 1, 1997
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Aeroassist Technology Workshop
Location: Pasadena, CA
Country: United States
Start Date: January 14, 1997
End Date: January 16, 1997
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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