Space Station multidisciplinary analysis capability - IDEAS2A computer-aided engineering tool now in use at NASA for systems engineering and integration analysis of the Space Station is described. This tool, called IDEAS2, combines the spacecraft-specific analysis software from NASA IDEAS (truss synthesizer, rigid body controls, plume impingement, orbital lifetime, orbit heat loads, and life support systems) with the interactive graphics, geometric database, solids modeler, structural and thermal analysis capability of the SDRC I-DEAS to obtain an integrated package suitable for Space Station design. This integrated package was applied to a very recent study of growth scenarios of the Space Station dual keel configuration, in which a comparison was made between designs using a combination of photovoltaic solar arrays and solar dynamic collectors, and those using only solar dynamic collectors.
Document ID
19860054109
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Baker, M. (Structural Dynamics Research Corp. San Diego, CA, United States)
Chiger, H. D. (Structural Dynamics Research Corp. San Diego, CA, United States)
Habermeyer, J. A. (Structural Dynamics Research Corp. San Diego, CA, United States)
Hipol, P. J. (Structural Dynamics Research Corp. San Diego, CA, United States)
Johnson, C. L. (Structural Dynamics Research Corp. San Diego, CA, United States)
Deryder, L. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 86-0954Report Number: AIAA PAPER 86-0954