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- W811841691 abstract "A technology readiness evaluation is made of the configurational, propulsion system, avionics, and materials/manufacturing methods which could be integrated to produce an economically viable SST by the year 2000. Aerodynamically, promising results are noted in the cases of arrow-wing planforms and blended wing/body cross sections, as well as in vortex flaps. In structures, metal matrix composites with high specific strength at high temperatures and thermoplastically formed/diffusion-bonded titanium alloy sandwich structures are identified as being of primary importance. Performance improvement prospects are also noted for engine efficiencies and sonic boom overpressures. The various technologies are envisaged as the bases for a two-engine, two-crew cockpit, 250-seat arrow-winged SST." @default.
- W811841691 created "2016-06-24" @default.
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- W811841691 date "1985-07-01" @default.
- W811841691 modified "2023-09-26" @default.
- W811841691 title "Readying technology for a super SST" @default.
- W811841691 hasPublicationYear "1985" @default.
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