SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE 3. BOEING MODEL 2707. FLIGHT CONTROLS AND HYDRAULICS SUBSYSTEM SPECIFICATION

Abstract

This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the flight controls and hydraulic subsystem for the prototype 2707-100 supersonic transport airplane. Differences between the prototype and production airplanes are described. This subsystem shall provide control of the airplane in response to pilot or guidance-navigation commands and furnish hydraulic power to the landing gear subsystem. This subsystem shall consist of primary flight controls, secondary flight controls, automatic flight controls and hydraulic power.

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Document Details

Document Type
Technical Report
Publication Date
Dec 31, 1966
Accession Number
AD0827604

Entities

People

  • E. See

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Sensors

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Computational Fluid Dynamics
  • Control Surfaces
  • Control Systems
  • Electric Motors
  • Electronic Components
  • Flight Control Systems
  • High Lift Devices
  • Inertial Navigation
  • Navigation
  • Swept Wings
  • Test And Evaluation
  • Transducers
  • Wing Flaps

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Systems Analysis and Design

Technology Areas

  • Hypersonics