NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Interactive design and analysis of future large spacecraft conceptsAn interactive computer aided design program used to perform systems level design and analysis of large spacecraft concepts is presented. Emphasis is on rapid design, analysis of integrated spacecraft, and automatic spacecraft modeling for lattice structures. Capabilities and performance of multidiscipline applications modules, the executive and data management software, and graphics display features are reviewed. A single user at an interactive terminal create, design, analyze, and conduct parametric studies of Earth orbiting spacecraft with relative ease. Data generated in the design, analysis, and performance evaluation of an Earth-orbiting large diameter antenna satellite are used to illustrate current capabilities. Computer run time statistics for the individual modules quantify the speed at which modeling, analysis, and design evaluation of integrated spacecraft concepts is accomplished in a user interactive computing environment.
Document ID
19820006403
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Garrett, L. B.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1981
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TP-1937
L-14739
Report Number: NASA-TP-1937
Report Number: L-14739
Meeting Information
Meeting: AIAA Thermophys. Conf.
Location: Palo Alto, CA
Country: United States
Start Date: June 23, 1981
End Date: June 25, 1981
Accession Number
82N14276
Funding Number(s)
PROJECT: RTOP 506-62-43-07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available