JTF17A-21B TURBOFAN ENGINE SPECIFICATION

Abstract

This specification establishes design and performance requirements for the Pratt and Whitney Aircraft JTF17A-21B 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 noted.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Aug 08, 1966
Accession Number
AD0804527

Entities

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Calorific Value
  • Control Systems
  • Engine Components
  • Engine Noise
  • Exhaust Gases
  • Exhaust Nozzles
  • Fuel Systems
  • High Pressure
  • High Pressure Compressors
  • Ignition
  • Ignition Systems
  • Measurement
  • Test And Evaluation
  • Test Facilities
  • Turbines

Fields of Study

  • Physics

Readers

  • Aerospace Engineering

Technology Areas

  • Hypersonics