JTF17A-21L TURBOFAN ENGINE SPECIFICATION

Abstract

This specification establishes design and performance requirements for the Pratt and Whitney Aircraft JTF17A-21L turbofan engine to be certificated in Phase 4 of the Supersonic Transport Program. Significant differences in the design and performance of the Phase 3 Flight Test Status engines for airplane flight testing are described.

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Document Details

Document Type
Technical Report
Publication Date
Aug 08, 1966
Accession Number
AD0804528

Entities

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Aircrafts
  • Airframes
  • Calorific Value
  • Control Systems
  • Distortion
  • Exhaust Gases
  • Exhaust Nozzles
  • Fuel Systems
  • High Pressure
  • Ignition
  • Ignition Systems
  • Measurement
  • Test And Evaluation
  • Test Facilities
  • Turbines
  • Turbofan Engines

Fields of Study

  • Physics

Readers

  • Aerospace Engineering

Technology Areas

  • Hypersonics