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.

Document Details

Document Type
Technical Report
Publication Date
Mar 10, 1966
Accession Number
AD0376675

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