SUPERSONIC TRANSPORT PROGRAM. PHASE II-C REPORT. FLIGHT CONTROLS AND HYDRAULICS SUBSYSTEM SPECIFICATION. SST BOEING MODEL 2707,

Abstract

This specification establishes the requirements for performance, design, test and qualification of the Flight Controls and Hydraulics Subsystem, as applied to the prototype preproduction airplanes. This subsystem shall provide control of the airplane in response to pilot or guidance-navigation system commands and furnish hydraulic power to the Landing Gear Subsystem, D6A10108-1. The 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
Jun 30, 1966
Accession Number
AD0805661

Entities

People

  • L. A. Hulsman

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

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

Readers

  • Aerospace Engineering
  • Aerospace Test and Evaluation

Technology Areas

  • Hypersonics