SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE 3 PROPOSAL. BOEING MODEL 2707. AIRFRAME SUBSYSTEM SPECIFICATION

Abstract

This specification establishes the requirements for performance, design, test, and qualification for the Airframe Subsystem as applied to the prototype model supersonic transport airplanes. 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.

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Document Details

Document Type
Technical Report
Publication Date
Sep 06, 1966
Accession Number
AD0804694

Entities

People

  • John Katzinski

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircrafts
  • Airframes
  • Control Surfaces
  • Corrosion Inhibition
  • Failure Mode And Effect Analysis
  • Fuselages
  • High Lift Devices
  • Horizontal Stabilizers
  • Landing Gear
  • Landing Gear Doors
  • Mechanics
  • Nose Wheels
  • Safety
  • Spars
  • Supersonic Transport Aircraft
  • Test And Evaluation

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Engineering
  • Aerospace Test and Evaluation

Technology Areas

  • Hypersonics