SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE 3. PROPOSAL. BOEING MODEL 2707. VOLUME 2-6-1. AIRFRAME DESIGN REPORT. PART A. WEIGHT AND BALANCE

Abstract

This report gives a detail weight breakdown of the proposed airplane and the design data and methods used in determining these weights. The report also includes moment of inertia, balance, and loading information. Supplement A provides weight data for the prototype airplane and Supplement B provides data for the domestic.

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Document Details

Document Type
Technical Report
Publication Date
Sep 06, 1966
Accession Number
AD0804726

Entities

People

  • E. M. Brown

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Control Surfaces
  • Control Systems
  • Floors
  • Fuel Systems
  • Fuselages
  • Horizontal Stabilizers
  • Inertial Navigation Systems
  • Jet Aircraft
  • Landing Gear
  • Navigation
  • Nose Wheels
  • Spars
  • Transport Aircraft

Readers

  • Aviation Science / Aeronautics.
  • Business Analytics
  • Control Systems Engineering.

Technology Areas

  • Hypersonics