COMMERCIAL SUPERSONIC TRANSPORT PROGRAM. PHASE II-C. INTERIM AIRCRAFT PERFORMANCE ASSESSMENT REPORT. PROPULSION CONTROLS PERFORMANCE SPECIFICATION.

Abstract

This specification describes the principal physical and functional characteristics of the control systems necessary to start, set, vary thrust, and stop the General Electric GE4/J5G engine. The design requirements are specified. Ground and flight tests to ensure that the control systems are satisfactory have been established. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of these requirements to production airplane design will be established after prototype flight testing. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 15, 1965
Accession Number
AD0804451

Entities

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Control Systems
  • Fixed Wing Aircraft
  • Flight Testing
  • Jet Aircraft
  • Production
  • Prototypes
  • Specifications
  • Supersonic Aircraft
  • Supersonic Transport Aircraft
  • Transport Ships
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow