SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE III PROPOSAL. 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 B-2707 supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. 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. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 06, 1966
Accession Number
AD0804705

Entities

People

  • E. See

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Airplanes
  • Automatic
  • Guidance
  • Hydraulic Power
  • Hydraulics
  • Landing Gear
  • Models
  • Navigation
  • Power
  • Production
  • Prototypes
  • Specifications
  • Supersonic Transport Aircraft
  • Transport Ships

Readers

  • Aerospace Engineering

Technology Areas

  • Hypersonics