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

Abstract

Contents: Engine Design; Engine Testing; Fan and High 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; Reliability; Safety; Thrust Indicating System; and Economic Studies.

Document Details

Document Type
Technical Report
Publication Date
Jan 11, 1967
Accession Number
AD0378925

Entities

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Engines
  • Aircrafts
  • Configuration Management
  • Engineering
  • Engines
  • Exhaust Systems
  • Reliability
  • Supersonic Transport Aircraft
  • Transport Aircraft
  • Value Engineering

Fields of Study

  • Physics

Readers

  • Aerospace Engineering

Technology Areas

  • Hypersonics