This specification establishes the requirements for performance, design, test, and qualification for the Airframe Subsystem as applied to the prototype model supersonic transport airplenes. The airframe subsystem consists of the fuselage, empennage, wing and control surfaces. Discrete differences between the prototype model supersonic transport airplanes and production airplanes are included in Supplement I. (Author)


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    Title :

    Supersonic Transport Development Program. Phase III Proposal. Boeing Model 2707. Airframe Subsystem Specification


    Contributors:

    Publication date :

    1966


    Size :

    75 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English