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- W2332263105 abstract "For the first time in this country, an airplane has been developed to both military and Federal Aviation Agency (FAA) requirements, with type certification as a requirement of the military contract. Although fundamentally an exploitation of proven state of the art, the 318,000-lb C-141 has many unusual features and represents the solution of several interesting development problems. Of chief interest are its cargo-handling features, the aerodynamic design of its modestly swept wing and of its T-tail, the derivation of its low-drag fuselage afterbody with full cross-section loadable opening, its stringent weight-control program, its long fan-duct nacelle design, its short nacelle inlets, its flight-station innovations for crew efficiency and comfort, and its unique main-landing-gear design. Rather substantial test programs are still in progress, mainly, by now, in the fatigue and flight areas. The C-141 received its FAA type certificate on January 29,1965." @default.
- W2332263105 created "2016-06-24" @default.
- W2332263105 creator A5017092667 @default.
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- W2332263105 date "1964-08-10" @default.
- W2332263105 modified "2023-09-26" @default.
- W2332263105 title "Development highlights of the c-141 starlifter" @default.
- W2332263105 doi "https://doi.org/10.2514/6.1964-596" @default.
- W2332263105 hasPublicationYear "1964" @default.
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