Research, design considerations, and technological problems of structures for winged aerospace vehicles
Research, design considerations, and technological problems of structures for winged aerospace vehicles
- New search for: Mathauser, E.E.
- New search for: Mathauser, E.E.
Types of vehicles considered are research aircraft characterized by X-15, re-entry glider representative of X-20 Dyna-Soar, and large hypersonic aircraft capable of sustained flight at hypersonic speed or having orbital capability; flight corridors and structural temperatures; hot structure and protected structure concept; structural concepts for cryogenic fueled vehicles; leading edge approaches; application of construction concepts for nonuniformly heated structures; insulating heat shield concept; other factors, such as flutter, fatigue, and materials selection.
Document information
Research, design considerations, and technological problems of structures for winged aerospace vehicles
NASA -- Univ Conf Science Technology Space Exploration -- Proc
Proceedings of the NASA -- University Conference on Science and Technology of Space Exploration ; 1962 Design
1962
12 pages
Conference paper
English
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