SUPERSONIC TRANSPORT AIRCRAFT ENGINE. PHASE II-B. DEVELOPMENT PROGRAM FUEL CONTROL SYSTEM STUDY. APPENDIX A.

Abstract

The objective of the current program was to continue the design and development of critical components, to analyze and implement any changes in control design resulting from changes in engine requirements, and to develop a control installation concept compatible with envelope limitations dictated by the engine installation.

Document Details

Document Type
Technical Report
Publication Date
Jun 30, 1965
Accession Number
AD0807389

Entities

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Aircraft Engines
  • Aircrafts
  • Control Systems
  • Cooperation
  • Engines
  • Jet Aircraft
  • Supersonic Aircraft
  • Supersonic Transport Aircraft
  • Transport Aircraft
  • Transport Ships
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Software Engineering

Technology Areas

  • Hypersonics