Computer Science – Performance
Scientific paper
Dec 1981
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1981saad....2.....r&link_type=abstract
Unknown
Computer Science
Performance
Aerospace Systems, Aerospace Vehicles, Design Analysis, Dynamic Loads, Loads (Forces), Structural Design Criteria, Hubble Space Telescope, Payloads, Space Shuttles, Spacecraft Design, Spacelab, Systems Engineering
Scientific paper
The achievement of an optimized design from the system standpoint under the low cost, high risk constraints of the present day environment was analyzed. Space Shuttle illustrates the requirement for an analysis approach that considers all major disciplines (coupling between structures control, propulsion, thermal, aeroelastic, and performance), simultaneously. The Space Shuttle and certain payloads, Space Telescope and Spacelab, are examined. The requirements for system analysis approaches and criteria, including dynamic modeling requirements, test requirements, control requirements, and the resulting design verification approaches are illustrated. A survey of the problem, potential approaches available as solutions, implications for future systems, and projected technology development areas are addressed.
Bullock T.
Holland W. B.
Kiefling L. A.
Kross D. A.
Ryan R. S.
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