Hypersonic vehicles are envisioned to require, in addition to carbon-carbon and ceramic-matrix composites for leading edges heated to above 2000 F, such 600 to 1800 F operating temperature materials as advanced Ti alloys, nickel aluminides, and metal-matrix composited; These possess the necessary low density and high strength and stiffness. The primary design drivers are maximum vehicle heating rate, total heat load, flight envelope, propulsion system type, mission life requirements and liquid hydrogen containment systems. Attention is presently given to aspects of these materials and structures requiring more intensive development.
Materials and Structures for Hypersonic Vehicles
1988
46 pages
Report
No indication
English
Materials and Structures for Hypersonic Vehicles
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