System analysis approach to deriving design criteria (loads) for Space Shuttle and its payloads. Volume 1: General statement of approach

Details System analysis approach to deriving design criteria (loads) for Space Shuttle and its payloads. Volume 1: General statement of approach System analysis approach to deriving design criteria (loads) for Space Shuttle and its payloads. Volume 1: General statement of approach

Dec 1981

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1981saad....1.....r&link_type=abstract

Unknown

Computer Science

Performance

Aerodynamic Loads, Hubble Space Telescope, Spacecraft Design, Spacelab, Structural Design Criteria, Systems Analysis, Cost Analysis, Engine Design, Launching Pads, Load Distribution (Forces), Spacecraft Construction Materials, Structural Weight

Scientific paper

Space shuttle, the most complex transportation system designed to date, illustrates the requirement for an analysis approach that considers all major disciplines simultaneously. Its unique cross coupling and high sensitivity to aerodynamic uncertainties and high performance requirements dictated a less conservative approach than those taken in programs. Analyses performed for the space shuttle and certain payloads, Space Telescope and Spacelab, are used a examples. These illustrate the requirements for system analysis approaches and criteria, including dynamic modeling requirements, test requirements control requirements and the resulting design verification approaches. A survey of the problem, potential approaches available as solutions, implications for future systems, and projected technology development areas are addressed.

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