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)
Supersonic Transport Development Program. Phase III Proposal. Boeing Model 2707. Airframe Subsystem Specification
1966
75 pages
Report
No indication
English