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Interactive design and analysis of future large spacecraft conceptsRecent developments in interactive computer-aided design and analysis of future large spacecraft concepts are presented. The primary emphases are on automatic spacecraft modeling for lattice (truss-like) structures and simplified multidiscipline design and analysis modules. Capabilities and performance of the twenty some applications modules, the executive and data management software, and graphics display features are reviewed. Data generated for an earth-orbiting large diameter (750 meter) antenna satellite are used to illustrate current capabilities. A single user at an interactive terminal can create, design, analyze, and conduct parametric studies of earth-orbiting spacecraft with relative ease. The approach is particularly useful in the conceptual design phase of advanced space missions when a multiplicity of concepts must be evaluated in a cost-effective and timely manner
Document ID
19810054752
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Garrett, L. B.
(NASA Langley Research Center Space Systems Div., Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
June 1, 1981
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 81-1177
Meeting Information
Meeting: Thermophysics Conference
Location: Palo Alto, CA
Start Date: June 23, 1981
End Date: June 25, 1981
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
81A39156
Distribution Limits
Public
Copyright
Other

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