One of the next steps in man's exploration of space is the development of a reusable space system capable of transporting men and equipment to near-earth orbits and returning them safely to earth. NASA's Space Shuttle Program is designed to achieve this goal in the 1970's with a reusable space orbiter and a reusable booster. This paper identifies the structural problems inherent in these craft and discusses the structural details of the orbiter design being studied by North American Rockwell's Space Division. In this Phase B study, which is being conducted under contract for NASA's Manned Spacecraft Center, cost is accorded primary consideration in all technical tradeoffs.
Space Shuttle Structural Design Concepts and Fabrication Problems
Sae Technical Papers
National Aeronautic and Space Engineering and Manufacturing Meeting ; 1970
1970-02-01
Conference paper
English
Structural dynamic problems of the space shuttle
AIAA | 1970
|Space shuttle structural design criteria development
NTRS | 1970
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