DEVELOPMENT OF A SUPERSONIC TRANSPORT AIRCRAFT ENGINE PHASE II-C.

Abstract

Contents: Engine Design; Engine Test; Compressor; Primary Combustor; Turbine; Augmentor; Exhaust System; Controls; Bearings and Seals; Fuels and Lubricants; Inlet System Compatibility; Noise; Mockups; Coordination; Maintainability; Value Engineering; Configuration Management; Quality Assurance; and Reliability.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jan 10, 1967
Accession Number
AD0378776

Entities

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Air Platforms
  • Human Systems

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Control Systems
  • Detectors
  • Engineering
  • Engineers
  • Exhaust Systems
  • Failure Mode And Effect Analysis
  • Gas Turbines
  • Heat Transfer
  • Ignition
  • Jet Aircraft
  • Plastic Explosives
  • Supersonic Transport Aircraft
  • Test Equipment
  • Test Facilities
  • Turbines

Fields of Study

  • Physics

Readers

  • Aerospace Engineering

Technology Areas

  • Hypersonics